The Project Gutenberg eBook ofThe Aeroplane SpeaksThis ebook is for the use of anyone anywhere in the United States and most other parts of the world at no cost and with almost no restrictions whatsoever. You may copy it, give it away or re-use it under the terms of the Project Gutenberg License included with this ebook or online atwww.gutenberg.org. If you are not located in the United States, you will have to check the laws of the country where you are located before using this eBook.Title: The Aeroplane SpeaksAuthor: H. BarberRelease date: February 1, 1997 [eBook #818]Most recently updated: January 27, 2021Language: EnglishCredits: Produced by Charles Keller, and David Widger*** START OF THE PROJECT GUTENBERG EBOOK THE AEROPLANE SPEAKS ***
This ebook is for the use of anyone anywhere in the United States and most other parts of the world at no cost and with almost no restrictions whatsoever. You may copy it, give it away or re-use it under the terms of the Project Gutenberg License included with this ebook or online atwww.gutenberg.org. If you are not located in the United States, you will have to check the laws of the country where you are located before using this eBook.
Title: The Aeroplane SpeaksAuthor: H. BarberRelease date: February 1, 1997 [eBook #818]Most recently updated: January 27, 2021Language: EnglishCredits: Produced by Charles Keller, and David Widger
Title: The Aeroplane Speaks
Author: H. Barber
Author: H. Barber
Release date: February 1, 1997 [eBook #818]Most recently updated: January 27, 2021
Language: English
Credits: Produced by Charles Keller, and David Widger
*** START OF THE PROJECT GUTENBERG EBOOK THE AEROPLANE SPEAKS ***
The reasons impelling me to write this book, the maiden effort of my pen, are, firstly, a strong desire to help the ordinary man to understand the Aeroplane and the joys and troubles of its Pilot; and, secondly, to produce something of PRACTICAL assistance to the Pilot and his invaluable assistant the Rigger. Having had some eight years' experience in designing, building, and flying aeroplanes, I have hopes that the practical knowledge I have gained may offset the disadvantage of a hand more used to managing the “joy-stick” than the dreadful haltings, the many side-slips, the irregular speed, and, in short, the altogether disconcerting ways of a pen.
The matter contained in the Prologue appeared in the Field of May 6th, 13th, 20th, and 27th, 1916, and is now reprinted by the kind permission of the editor, Sir Theodore Cook.
I have much pleasure in also acknowledging the kindness of Mr. C. G. Grey, editor of the Aeroplane, to whom I am indebted for the valuable illustrations reproduced at the end of this book.
CONTENTSMOTIVETHE AEROPLANE SPEAKSPROLOGUEPART I. THE ELEMENTARY PRINCIPLES AIR THEIR GRIEVANCESPART II. THE PRINCIPLES, HAVING SETTLED THEIR DIFFERENCES, FINISH THEPART III. THE GREAT TESTPART IV. 'CROSS COUNTRYCHAPTER I. FLIGHTCHAPTER II. STABILITY AND CONTROLCHAPTER III. RIGGINGCHAPTER IV. THE PROPELLER, OR “AIR-SCREW”CHAPTER V. MAINTENANCEGLOSSARYFOOTNOTES
CONTENTS
MOTIVE
THE AEROPLANE SPEAKS
PROLOGUE
PART I. THE ELEMENTARY PRINCIPLES AIR THEIR GRIEVANCES
PART II. THE PRINCIPLES, HAVING SETTLED THEIR DIFFERENCES, FINISH THE
PART III. THE GREAT TEST
PART IV. 'CROSS COUNTRY
CHAPTER I. FLIGHT
CHAPTER II. STABILITY AND CONTROL
CHAPTER III. RIGGING
CHAPTER IV. THE PROPELLER, OR “AIR-SCREW”
CHAPTER V. MAINTENANCE
GLOSSARY
FOOTNOTES
The Lecture Hall at the Royal Flying Corps School for Officers was deserted. The pupils had dispersed, and the Officer Instructor, more fagged than any pupil, was out on the aerodrome watching the test of a new machine.
Deserted, did I say? But not so. The lecture that day had been upon the Elementary Principles of Flight, and they lingered yet. Upon the Blackboard was the illustration you see in the frontispiece.
“I am the side view of a Surface,” it said, mimicking the tones of the lecturer. “Flight is secured by driving me through the air at an angle inclined to the direction of motion.”
“Quite right,” said the Angle. “That's me, and I'm the famous Angle of Incidence.”
“And,” continued the Surface, “my action is to deflect the air downwards, and also, by fleeing from the air behind, to create a semi-vacuum or rarefied area over most of the top of my surface.”
“This is where I come in,” a thick, gruff voice was heard, and went on: “I'm the Reaction. You can't have action without me. I'm a very considerable force, and my direction is at right-angles to you,” and he looked heavily at the Surface. “Like this,” said he, picking up the chalk with his Lift, and drifting to the Blackboard.
“I act in the direction of the arrow R, that is, more or less, for the direction varies somewhat with the Angle of Incidence and the curvature of the Surface; and, strange but true, I'm stronger on the top of the Surface than at the bottom of it. The Wind Tunnel has proved that by exhaustive research—and don't forget how quickly I can grow! As the speed through the air increases my strength increases more rapidly than you might think—approximately, as the Square of the Speed; so you see that if the Speed of the Surface through the air is, for instance, doubled, then I am a good deal more than doubled. That's because I am the result of not only the mass of air displaced, but also the result of the Speed with which the Surface engages the Air. I am a product of those two factors, and at the speeds at which Aeroplanes fly to-day, and at the altitudes and consequent density of air they at present experience, I increase at about the Square of the Speed.
“Oh, I'm a most complex and interesting personality, I assure you—in fact, a dual personality, a sort of aeronautical Dr. Jekyll and Mr. Hyde. There's Lift, my vertical part or COMPONENT, as those who prefer long words would say; he always acts vertically upwards, and hates Gravity like poison. He's the useful and admirable part of me. Then there's Drift, my horizontal component, sometimes, though rather erroneously, called Head Resistance; he's a villain of the deepest dye, and must be overcome before flight can be secured.”
“And I,” said the Propeller, “I screw through the air and produce the Thrust. I thrust the Aeroplane through the air and overcome the Drift; and the Lift increases with the Speed and when it equals the Gravity of Weight, then—there you are—Flight! And nothing mysterious about it at all.”
“I hope you'll excuse me interrupting,” said a very beautiful young lady, “my name is Efficiency, and, while no doubt, all you have said is quite true, and that, as my young man the Designer says, `You can make a tea-tray fly if you slap on Power enough,' I can assure you that I'm not to be won quite so easily.”
“Well,” eagerly replied the Lift and the Thrust, “let's be friends. Do tell us what we can do to help you to overcome Gravity and Drift with the least possible Power. That obviously seems the game to play, for more Power means heavier engines, and that in a way plays into the hands of our enemy, Gravity, besides necessitating a larger Surface or Angle to lift the Weight, and that increases the Drift.”
“Very well,” from Efficiency, “I'll do my best, though I'm so shy, and I've just had such a bad time at the Factory, and I'm terribly afraid you'll find it awfully dry.”
“Buck up, old dear!” This from several new-comers, who had just appeared. “We'll help you,” and one of them, so lean and long that he took up the whole height of the lecture room, introduced himself.
“I'm the High Aspect Ratio,” he said, “and what we have got to do to help this young lady is to improve the proportion of Lift to Drift. The more Lift we can get for a certain area of Surface, the greater the Weight the latter can carry; and the less the Drift, then the less Thrust and Power required to overcome it. Now it is a fact that, if the Surface is shaped to have the greatest possible span, i.e., distance from wing-tip to wing-tip, it then engages more air and produces both a maximum Reaction and a better proportion of Lift to Drift.
“That being so, we can then well afford to lose a little Reaction by reducing the Angle of Incidence to a degree giving a still better proportion of Lift to Drift than would otherwise be the case; for you must understand that the Lift-Drift Ratio depends very much upon the size of the Angle of Incidence, which should be as small as possible within certain limits. So what I say is, make the surface of Infinite Span with no width or chord, as they call it. That's all I require, I assure you, to make me quite perfect and of infinite service to Miss Efficiency.”
“That's not practical politics,” said the Surface. “The way you talk one would think you were drawing L400 a year at Westminster, and working up a reputation as an Aeronautical Expert. I must have some depth and chord to take my Spars and Ribs, and again, I must have a certain chord to make it possible for my Camber (that's curvature) to be just right for the Angle of Incidence. If that's not right the air won't get a nice uniform compression and downward acceleration from my underside, and the rarefied `suction' area over the top of me will not be as even and clean in effect as it might be. That would spoil the Lift-Drift Ratio more than you can help it. Just thrust that chalk along, will you? and the Blackboard will show you what I mean.”
“Well,” said the Aspect Ratio, “have it your own way, though I'm sorry to see a pretty young lady like Efficiency compromised so early in the game.”
“Look here,” exclaimed a number of Struts, “we have got a brilliant idea for improving the Aspect Ratio,” and with that they hopped up on to the Spars. “Now,” excitedly, “place another Surface on top of us. Now do you see? There is double the Surface, and that being so, the proportion of Weight to Surface area is halved. That's less burden of work for the Surface, and so the Spars need not be so strong and so deep, which results in not so thick a Surface. That means the Chord can be proportionately decreased without adversely affecting the Camber. With the Chord decreased, the Span becomes relatively greater, and so produces a splendid Aspect Ratio, and an excellent proportion of Lift to Drift.”
“I don't deny that they have rather got me there,” said the Drift, “but all the same, don't forget my increase due to the drift of the Struts and their bracing wires.”
“Yes, I dare say,” replied the Surface, “but remember that my Spars are less deep than before, and consequently I am not so thick now, and shall for that reason also be able to go through the air with a less proportion of Drift to Lift.”
“Remember me also, please,” croaked the Angle of Incidence. “Since the Surface has now less weight to carry for its area, I may be set at a still lesser and finer Angle. That means less Drift again. We are certainly getting on splendidly! Show us how it looks now, Blackboard.” And the Blackboard obligingly showed them as follows:
“Well, what do you think of that?” they all cried to the Drift.
“You think you are very clever,” sneered the Drift. “But you are not helping Efficiency as much as you think. The suction effect on the top of the lower Surface will give a downward motion to the air above it and the result will be that the bottom of the top Surface will not secure as good a Reaction from the air as would otherwise be the case, and that means loss of Lift; and you can't help matters by increasing the gap between the surfaces because that means longer Struts and Wires, and that in itself would help me, not to speak of increasing the Weight. You see it's not quite so easy as you thought.”
At this moment a hiccough was heard, and a rather fast and rakish-looking chap, named Stagger, spoke up. “How d'ye do, miss,” he said politely to Efficiency, with a side glance out of his wicked old eye. “I'm a bit of a knut, and without the slightest trouble I can easily minimize the disadvantage that old reprobate Drift has been frightening you with. I just stagger the top Surface a bit forward, and no longer is that suction effect dead under it. At the same time I'm sure the top Surface will kindly extend its Span for such distance as its Spars will support it without the aid of Struts. Such extension will be quite useful, as there will be no Surface at all underneath it to interfere with the Reaction above.” And the Stagger leaned forward and picked up the Chalk, and this is the picture he drew:
Said the Blackboard, “That's not half bad! It really begins to look something like the real thing, eh?”
“The real thing, is it?” grumbled Drift. “Just consider that contraption in the light of any one Principle, and I warrant you will not find one of them applied to perfection. The whole thing is nothing but a Compromise.” And he glared fixedly at poor Efficiency.
“Oh, dear! Oh, dear!” she cried. “I'm always getting into trouble. What WILL the Designer say?”
“Never mind, my dear,” said the Lift-Drift Ratio, consolingly. “You are improving rapidly, and quite useful enough now to think of doing a job of work.”
“Well, that's good news,” and Efficiency wiped her eyes with her Fabric and became almost cheerful. “Suppose we think about finishing it now? There will have to be an Engine and Propeller, won't there? And a body to fix them in, and tanks for oil and petrol, and a tail, and,” archly, “one of those dashing young Pilots, what?”
“Well, we are getting within sight of those interesting Factors,” said the Lift-Drift Ratio, “but first of all we had better decide upon the Area of the Surfaces, their Angle of Incidence and Camber. If we are to ascend as quickly as possible the Aeroplane must be SLOW in order to secure the best possible Lift-Drift Ratio, for the drift of the struts wires, body, etc., increases approximately as the square of the speed, but it carries with it no lift as it does in the case of the Surface. The less speed then, the less such drift, and the better the Aeroplane's proportion of lift to drift; and, being slow, we shall require a LARGE SURFACE in order to secure a large lift relative to the weight to be carried. We shall also require a LARGE ANGLE OF INCIDENCE relative to the horizontal, in order to secure a proper inclination of the Surface to the direction of motion, for you must remember that, while we shall fly upon an even keel and with the propeller thrust horizontal (which is its most efficient attitude), our flight path, which is our direction of motion, will be sloping upwards, and it will therefore be necessary to fix the Surface to the Aeroplane at a very considerable angle relative to the horizontal Propeller Thrust in order to secure a proper angle to the upwards direction of motion. Apart from that, we shall require a larger Angle of Incidence than in the case of a machine designed purely for speed, and that means a correspondingly LARGE CAMBER.
“On the other hand, if we are thinking merely of Speed, then a SMALL SURFACE, just enough to lift the weight off the ground, will be best, also a SMALL ANGLE to cut the Drift down and that, of course, means a relatively SMALL CAMBER.
“So you see the essentials for CLIMB or quick ascent and for SPEED are diametrically opposed. Now which is it to be?”
“Nothing but perfection for me,” said Efficiency. “What I want is Maximum Climb and Maximum Speed for the Power the Engine produces.”
And each Principle fully agreed with her beautiful sentiments, but work together they would not.
The Aspect Ratio wanted infinite Span, and hang the Chord.
The Angle of Incidence would have two Angles and two Cambers in one, which was manifestly absurd; the Surface insisted upon no thickness whatever, and would not hear of such things as Spars and Ribs; and the Thrust objected to anything at all likely to produce Drift, and very nearly wiped the whole thing off the Blackboard.
There was, indeed, the makings of a very pretty quarrel when the Letter arrived. It was about a mile long, and began to talk at once.
“I'm from the Inventor,” he said, and hope rose in the heart of each heated Principle. “It's really absurdly simple. All the Pilot has to do is to touch a button, and at his will, VARY the area of the Surface, the Angle of Incidence, and the Camber! And there you are—Maximum Climb or Maximum Speed as required! How does that suit you?”
“That suits us very well,” said the Surface, “but, excuse me asking, how is it done without apparatus increasing the Drift and the Weight out of all reason? You won't mind showing us your Calculations, Working Drawings, Stress Diagrams, etc., will you?”
Said the Letter with dignity, “I come from an Inventor so brilliantly clever as to be far above the unimportant matters you mention. He is no common working man, sir! He leaves such things to Mechanics. The point is, you press a button and——”
“Look here,” said a Strut, rather pointedly, “where do you think you are going, anyway?”
“Well,” from the Letter, “as a matter of fact, I'm not addressed yet, but, of course, there's no doubt I shall reach the very highest quarters and absolutely revolutionize Flight when I get there.”
Said the Chalk, “I'll address you, if that's all you want; now drift along quickly!” And off went the Letter to The Technical Editor, “Daily Mauler,” London.
And a League was formed, and there were Directors with Fees, and several out-of-service Tin Hats, and the Man-who-takes-the-credit, and a fine fat Guinea-pig, and all the rest of them. And the Inventor paid his Tailor and had a Hair-Cut, and is now a recognized Press Expert—but he is still waiting for those Mechanics!
“I'm afraid,” said the Slide-rule, who had been busy making those lightning-like automatic calculations for which he is so famous, “it's quite impossible to fully satisfy all of you, and it is perfectly plain to me that we shall have to effect a Compromise and sacrifice some of the Lift for Speed.”
Thud! What was that?
Efficiency had fainted dead away! The last blow had been too much for her. And the Principles gathered mournfully round, but with the aid of the Propeller Slip1and a friendly lift from the Surface she was at length revived and regained a more normal aspect.
Said the Stagger with a raffish air, “My dear young lady, I assure you that from the experiences of a varied career, I have learned that perfection is impossible, and I am sure the Designer will be quite satisfied if you become the Most Efficient Compromise.”
“Well, that sounds so common sense,” sighed Efficiency, “I suppose it must be true, and if the Designer is satisfied, that's all I really care about. Now do let's get on with the job.”
So the Chalk drew a nice long slim body to hold the Engine and the tanks, etc., with room for the Pilot's and Passenger's seats, and placed it exactly in the middle of the Biplane. And he was careful to make its position such that the Centre of Gravity was a little in advance of the Centre of Lift, so that when the Engine was not running and there was consequently no Thrust, the Aeroplane should be “nose-heavy” just to the right degree, and so take up a natural glide to Earth—and this was to help the Pilot and relieve him of work and worry, should he find himself in a fog or a cloud. And so that this tendency to glide downwards should not be in evidence when the Engine was running and descent not desired, the Thrust was placed a little below the Centre of Drift or Resistance. In this way it would in a measure pull the nose of the Aeroplane up and counterbalance the “nose-heavy” tendency.
And the Engine was so mounted that when the Propeller-Thrust was horizontal, which is its most efficient position, the Angle of Incidence and the Area of the surfaces were just sufficient to give a Lift a little in excess of the Weight. And the Camber was such that, as far as it was concerned, the Lift-Drift Ratio should be the best possible for that Angle of Incidence. And a beautifully simple under-carriage was added, the outstanding features of which were simplicity, strength, light-weight, and minimum drift. And, last of all, there was the Elevator, of which you will hear more by-and-by. And this is what it looked like then:
And Efficiency, smiling, thought that it was not such a bad compromise after all and that the Designer might well be satisfied.
“Now,” said she, “there's just one or two points I'm a bit hazy about. It appears that when the Propeller shaft is horizontal and so working in its most efficient attitude, I shall have a Lift from the Surfaces slightly in excess of the Weight. That means I shall ascend slightly, at the same time making nearly maximum speed for the power and thrust. Can't I do better than that?”
“Yes, indeed,” spoke up the Propeller, “though it means that I must assume a most undignified attitude, for helicopters2I never approved of. In order to ascend more quickly the Pilot will deflect the Elevator, which, by the way, you see hinged to the Tail. By that means he will force the whole Aeroplane to assume a greater Angle of Incidence. And with greater Angle, the Lift will increase, though I'm sorry to say the Drift will increase also. Owing to the greater Drift, the Speed through the air will lessen, and I'm afraid that won't be helpful to the Lift; but I shall now be pointing upwards, and besides overcoming the Drift in a forward direction I shall be doing my best to haul the Aeroplane skywards. At a certain angle known as the Best Climbing Angle, we shall have our Maximum Margin of Lift, and I'm hoping that may be as much as almost a thousand feet altitude a minute.”
“Then, if the Pilot is green, my chance will come,” said the Maximum Angle of Incidence. “For if the Angle is increased over the Best Climbing Angle, the Drift will rush up; and the Speed, and with it the Lift, will, when my Angle is reached, drop to a point when the latter will be no more than the Weight. The Margin of Lift will have entirely disappeared, and there we shall be, staggering along at my tremendous angle, and only just maintaining horizontal flight.”
“And then with luck I'll get my chance,” said the Drift. “If he is a bit worse than green, he'll perhaps still further increase the Angle. Then the Drift, largely increasing, the Speed, and consequently the Lift, will become still less, i.e., less than the Weight, and then—what price pancakes,3eh?”
“Thank you,” from Efficiency, “that was all most informing. And now will you tell me, please, how the greatest Speed may be secured?”
“Certainly, now it's my turn,” piped the Minimum Angle of Incidence. “By means of the Elevator, the Pilot places the Aeroplane at my small Angle, at which the Lift only just equals the Weight, and, also, at which we shall make greater speed with no more Drift than before. Then we get our greatest Speed, just maintaining horizontal flight.”
“Yes; though I'm out of the horizontal and thrusting downwards,” grumbled the Propeller, “and that's not efficient, though I suppose it's the best we can do until that Inventor fellow finds his Mechanics.”
“Thank you so much,” said Efficiency. “I think I have now at any rate an idea of the Elementary Principles of Flight, and I don't know that I care to delve much deeper, for sums always give me a headache; but isn't there something about Stability and Control? Don't you think I ought to have a glimmering of them too?”
“Well, I should smile,” said a spruce Spar, who had come all the way from America. “And that, as the Lecturer says, `will be the subject of our next lecture,' so be here again to-morrow, and you will be glad to hear that it will be distinctly more lively than the subject we have covered to-day.”
JOB
Another day had passed, and the Flight Folk had again gathered together and were awaiting the arrival of Efficiency who, as usual, was rather late in making an appearance.
The crowd was larger than ever, and among the newcomers some of the most important were the three Stabilities, named Directional, Longitudinal, and Lateral, with their assistants, the Rudder, Elevator, and Ailerons. There was Centrifugal Force, too, who would not sit still and created a most unfavourable impression, and Keel-Surface, the Dihedral Angle, and several other lesser fry.
“Well,” said Centrifugal Force, “I wish this Efficiency I've heard so much about would get a move on. Sitting still doesn't agree with me at all. Motion I believe in. There's nothing like motion—the more the better.”
“We are entirely opposed to that,” objected the three Stabilities, all in a breath. “Unless it's in a perfectly straight line or a perfect circle. Nothing but perfectly straight lines or, upon occasion, perfect circles satisfy us, and we are strongly suspicious of your tendencies.”
“Well, we shall see what we shall see,” said the Force darkly. “But who in the name of blue sky is this?”
And in tripped Efficiency, in a beautifully “doped” dress of the latest fashionable shade of khaki-coloured fabric, a perfectly stream-lined bonnet, and a bewitching little Morane parasol,4smiling as usual, and airily exclaiming, “I'm so sorry I'm late, but you see the Designer's such a funny man. He objects to skin friction,5and insisted upon me changing my fabric for one of a smoother surface, and that delayed me. Dear me, there are a lot more of us to-day, aren't there? I think I had better meet one at a time.” And turning to Directional Stability, she politely asked him what he preferred to do.
“My purpose in life, miss,” said he, “is to keep the Aeroplane on its course, and to achieve that there must be, in effect, more Keel-Surface behind the Vertical Turning Axis than there is in front of it.”
Efficiency looking a little puzzled, he added: “Just like a weathercock, and by Keel-Surface I mean everything you can see when you view the Aeroplane from the side of it—the sides of the body, struts, wires, etc.”
“Oh, now I begin to see light,” said she: “but just exactly how does it work?”
“I'll answer that,” said Momentum. “When perhaps by a gust of air the Aeroplane is blown out of its course and points in another direction, it doesn't immediately fly off on that new course. I'm so strong I pull it off the new course to a certain extent, and towards the direction of the old course. And so it travels, as long as my strength lasts, in a more or less sideways position.”
“Then,” said the Keel-Surface, “I get a pressure of air all on one side, and as there is, in effect, most of me towards the tail, the latter gets pressed sideways, and the Aeroplane thus tends to assume its first position and course.”
“I see,” said Efficiency, and, daintily holding the Chalk, she approached the Blackboard. “Is this what you mean?”
“Yes, that's right enough,” said the Keel-Surface, “and you might remember, too, that I always make the Aeroplane nose into the gusts rather than away from them.”
“If that was not the case,” broke in Lateral Stability, and affecting the fashionable Flying Corps stammer, “it would be a h-h-h-o-r-rible affair! If there were too much Keel-Surface in front, then that gust would blow the Aeroplane round the other way a very considerable distance. And the right-hand Surface being on the outside of the turn would have more speed, and consequently more Lift, than the Surface on the other side. That means a greater proportion of the Lift on that side, and before you could say Warp to the Ailerons over the Aeroplane would go—probable result a bad side-slip”
“And what can the Pilot do to save such a situation as that?” said Efficiency.
“Well,” replied Lateral Stability, “he will try to turn the Aeroplane sideways and back to an even keel by means of warping the Ailerons or little wings which are hinged on to the Wing-tips, and about which you will hear more later on; but if the side-slip is very bad he may not be able to right the Aeroplane by means of the Ailerons, and then the only thing for him to do is to use the Rudder and to turn the nose of the Aeroplane down and head-on to the direction of motion. The Aeroplane will then be meeting the air in the direction it is designed to do so, and the Surfaces and also the controls (the Rudder, Ailerons, and Elevator) will be working efficiently; but its attitude relative to the earth will probably be more or less upside-down, for the action of turning the Aeroplane's nose down results, as you will see by the illustration B, in the right wing, which is on the outside of the circle. travelling through the air with greater speed than the left-hand wing. More Speed means more Lift, so that results in overturning the Aeroplane still more; but now it is, at any rate, meeting the air as it is designed to meet it, and everything is working properly. It is then only necessary to warp the Elevator, as shown in illustration C, in order to bring the Aeroplane into a proper attitude relative to the earth.”
“Ah!” said the Rudder, looking wise, “it's in a case like that when I become the Elevator and the Elevator becomes me.”
“That's absurd nonsense,” said the Blackboard, “due to looseness of thought and expression.”
“Well,” replied the Rudder, “when 'the Aeroplane is in position A and I am used, then I depress or ELEVATE the nose of the machine; and, if the Elevator is used, then it turns the Aeroplane to right or left, which is normally my function. Surely our roles have changed one with the other, and I'm then the Elevator and the Elevator is me!”
Said Lateral Stability to the Rudder, “That's altogether the wrong way of looking at it, though I admit”—and this rather sarcastically—“that the way you put it sounds rather fine when you are talking of your experiences in the air to those 'interested in aviation' but knowing little about it; but it won't go down here! You are a Controlling Surface designed to turn the Aeroplane about its vertical axis, and the Elevator is a Controlling Surface designed to turn the Aeroplane about its lateral axis. Those are your respective jobs, and you can't possibly change them about. Such talk only leads to confusion, and I hope we shall hear no more of it.”
“Thanks,” said Efficiency to Lateral Stability. “And now, please, will you explain your duties?”
“My duty is to keep the Aeroplane horizontal from Wing-tip to Wing-tip. First of all, I sometimes arrange with the Rigger to wash-out, that is decrease, the Angle of Incidence on one side of the Aeroplane, and to effect the reverse condition, if it is not too much trouble, on the other side.”
“But,” objected Efficiency, “the Lift varies with the Angle of Incidence, and surely such a condition will result in one side of the Aeroplane lifting more than the other side?'
“That's all right,” said the Propeller, “it's meant to off-set the tendency of the Aeroplane to turn over sideways in the opposite direction to which I revolve.”
“That's quite clear, though rather unexpected; but how do you counteract the effect of the gusts when they try to overturn the Aeroplane sideways?” said she, turning to Lateral Stability again.
“Well,” he replied, rather miserably, “I'm not nearly so perfect as the Longitudinal and Directional Stabilities. The Dihedral Angle—that is, the upward inclination of the Surfaces towards their wing-tips—does what it can for me, but, in my opinion, it's a more or less futile effort. The Blackboard will show you the argument.” And he at once showed them two Surfaces, each set at a Dihedral Angle like this:
“Please imagine,” said the Blackboard, “that the top V is the front view of a Surface flying towards you. Now if a gust blows it into the position of the lower V you see that the horizontal equivalent of the Surface on one side becomes larger, and on the other side it becomes smaller. That results in more Lift on the lower side and less on the higher side, and if the V is large enough it should produce such a difference in the Lift of one side to the other as to quickly turn the Aeroplane back to its former and normal position.”
“Yes,” said the Dihedral Angle, “that's what would happen if they would only make me large enough; but they won't do it because it would too greatly decrease the horizontal equivalent, and therefore the Lift, and incidentally it would, as Aeroplanes are built to-day, produce an excess of Keel Surface above the turning axis, and that in itself would spoil the Lateral Stability. The Keel Surface should be equally divided above and below the longitudinal turning axis (upon which the Aeroplane rolls sideways), or the side upon which there is an excess will get blown over by the gusts. It strikes me that my future isn't very promising, and about my only chance is when the Junior Draughtsman makes a mistake, as he did the other day. And just think of it, they call him a Designer now that he's got a job at the Factory! What did he do? Why, he calculated the weights wrong and got the Centre of Gravity too high, and they didn't discover it until the machine was built. Then all they could do was to give me a larger Angle. That dropped the bottom of the V lower down, and as that's the centre of the machine, where all the Weight is, of course that put the Centre of Gravity in its right place. But now there is too much Keel Surface above, and the whole thing's a Bad Compromise, not at all like Our Efficiency.”
And Efficiency, blushing very prettily at the compliment, then asked, “And how does the Centre of Gravity affect matters?”
“That's easy,” said Grandfather Gravity. “I'm so heavy that if I am too low down I act like a pendulum and cause the Aeroplane to roll about sideways, and if I am too high I'm like a stick balanced on your finger, and then if I'm disturbed, over I go and the Aeroplane with me; and, in addition to that, there are the tricks I play with the Aeroplane when it's banked up,6i.e., tilted sideways for a turn, and Centrifugal Force sets me going the way I'm not wanted to go. No; I get on best with Lateral Stability when my Centre is right on the centre of Drift, or, at any rate, not much below it.” And with that he settled back into the Lecturer's Chair and went sound asleep again, for he was so very, very old, in fact the father of all the Principles.
And the Blackboard had been busy, and now showed them a picture of the Aeroplane as far as they knew it, and you will see that there is a slight Dihedral Angle, and also, fixed to the tail, a vertical Keel Surface or fin, as is very often the case in order to ensure the greater effect of such surface being behind the vertical turning axis.
But Efficiency, growing rather critical with her newly gained knowledge, cried out: “But where's the horizontal Tail Surface? It doesn't look right like that!”
“This is when I have the pleasure of meeting you, my dear,” said Longitudinal Stability. “Here's the Tail Surface,” he said, “and in order to help me it must be set IN EFFECT at a much less Angle of Incidence than the Main Surface. To explain we must trouble the Blackboard again,” and this was his effort:
“I have tried to make that as clear as possible,” he said. “It may appear a bit complicated at first, but if you will take the trouble to look at it for a minute you will find it quite simple. A is the normal and proper direction of motion of the Aeroplane, but, owing to a gust of air, it takes up the new nose-down position. Owing to Momentum, however, it does not fly straight along in that direction, but moves more or less in the direction B, which is the resultant of the two forces, Momentum and Thrust. And so you will note that the Angle of Incidence, which is the inclination of the Surfaces to the Direction of Motion, has decreased, and of course the Lift decreases with it. You will also see, and this is the point, that the Tail Surface has lost a higher proportion of its Angle, and consequently its Lift, than has the Main Surface. Then, such being the case, the Tail must fall and the Aeroplane assume its normal position again, though probably at a slightly lower altitude.”
“I'm afraid I'm very stupid,” said Efficiency, “but please tell me why you lay stress upon the words 'IN EFFECT.'”
“Ah! I was wondering if you would spot that,” he replied. “And there is a very good reason for it. You see, in some Aeroplanes the Tail Surface may be actually set at the same Angle on the machine as the Main Surface, but owing to the air being deflected downwards by the front Main Surface it meets the Tail Surface at a lesser angle, and indeed in some cases at no angle at all. The Tail is then for its surface getting less Lift than the Main Surface, although set at the same angle on the machine. It may then be said to have IN EFFECT a less Angle of Incidence. I'll just show you on the Blackboard.”
“And now,” said Efficiency, “I have only to meet the Ailerons and the Rudder, haven't I?”
“Here we are,” replied the Ailerons, or little wings. “Please hinge us on to the back of the Main Surfaces, one of us at each Wing-tip, and join us up to the Pilot's joystick by means of the control cables. When the Pilot wishes to tilt the Aeroplane sideways, he will move the stick and depress us upon one side, thus giving us a larger Angle of Incidence and so creating more Lift on that side of the Aeroplane; and, by means of a cable connecting us with the Ailerons on the other side of the Aeroplane, we shall, as we are depressed, pull them up and give them a reverse or negative Angle of Incidence, and that side will then get a reverse Lift or downward thrust, and so we are able to tilt the Aeroplane sideways.
“And we work best when the Angle of Incidence of the Surface in front of us is very small, for which reason it is sometimes decreased or washed-out towards the Wing-tips. The reason of that is that by the time the air reaches us it has been deflected downwards—the greater the Angle of Incidence the more it is driven downwards—and in order for us to secure a Reaction from it, we have to take such a large Angle of Incidence that we produce a poor proportion of Lift to Drift; but the smaller the Angle of the Surface in front of us the less the air is deflected downwards, and consequently the less Angle is required of us, and the better our proportion of Lift to Drift, which, of course, makes us much more effective Controls.”
“Yes,” said the Lateral and Directional Stabilities in one voice, “that's so, and the wash-out helps us also, for then the Surfaces towards their Wing-tips have less Drift or 'Head-Resistance,' and consequently the gusts will affect them and us less; but such decreased Angle of Incidence means decreased Lift as well as Drift, and the Designer does not always care to pay the price.”
“Well,” said the Ailerons, “if it's not done it will mean more work for the Rudder, and that won't please the Pilot.”
“Whatever do you mean?” asked Efficiency. “What can the Rudder have to do with you?”
“It's like this,” they replied: “when we are deflected downwards we gain a larger Angle of Incidence and also enter an area of compressed air, and so produce more Drift than those of us on the other side of the Aeroplane, which are deflected upwards into an area of rarefied air due to the SUCTION effect (though that term is not academically correct) on the top of the Surface. If there is more Drift, i.e., Resistance, on one side of the Aeroplane than on the other side, then of course it will turn off its course, and if that difference in Drift is serious, as it will very likely be if there is no wash-out, then it will mean a good deal of work for the Rudder in keeping the Aeroplane on its course, besides creating extra Drift in doing so.”
“I think, then,” said Efficiency, “I should prefer to have that wash-out,7and my friend the Designer is so clever at producing strength of construction for light weight, I'm pretty sure he won't mind paying the price in Lift. And now let me see if I can sketch the completed Aeroplane.”
“Well, I hope that's all as it should be,” she concluded, “for to-morrow the Great Test in the air is due.”