قراءة كتاب The Theory and Practice of Model Aeroplaning

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The Theory and Practice of Model Aeroplaning

The Theory and Practice of Model Aeroplaning

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دار النشر: Project Gutenberg
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THE THEORY AND PRACTICE
OF
MODEL AEROPLANING

BY
V.E. JOHNSON, M.A.

AUTHOR OF
'THE BEST SHAPE FOR AN AIRSHIP,' 'SOARING FLIGHT,'
'HOW TO ADVANCE THE SCIENCE OF AERONAUTICS,'
'HOW TO BUILD A MODEL AEROPLANE,' ETC.

"Model Aeroplaning is an Art in itself"

London
E. & F.N. SPON, Ltd., 57 HAYMARKET
New York
SPON & CHAMBERLAIN, 123 LIBERTY STREET
1910


PREFACE

The object of this little book is not to describe how to construct some particular kind of aeroplane; this has been done elsewhere: but to narrate in plain language the general practice and principles of model aeroplaning.

There is a science of model aeroplaning—just as there is a science of model yachting and model steam and electric traction, and an endeavour is made in the following pages to do in some measure for model aeroplanes what has already been done for model yachts and locomotives. To achieve the best results, theory and practice must go hand in hand.

From a series of carefully conducted experiments empirical formulæ can be obtained which, combined later with mathematical induction and deduction, may lead, not only to a more accurate and generalized law than that contained in the empirical formula, but to valuable deductions of a totally new type, embodying some general law hitherto quite unknown by experimentalists, which in its turn may serve as a foundation or stepping stone for suggesting other experiments and empirical formulæ which may be of especial importance, to be treated in their turn like their predecessor. By "especial importance," I mean not only to "model," but "Aeroplaning" generally.

As to the value of experiments on or with models with respect to full-sized machines, fifteen years ago I held the opinion that they were a very doubtful factor. I have since considerably modified that view, and now consider that experiments with models—if properly carried out, and given due, not undue, weight—both can and will be of as much use to the science of Aeronautics as they have already proved themselves to be in that of marine engineering.

The subject of model propellers and motors has been somewhat fully dealt with, as but little has been published (in book form, at any rate) on these all-important departments. On similar grounds the reasons why and how a model aeroplane flies have been practically omitted, because these have been dealt with more or less in every book on heavier-than-air machines.

Great care has been exercised in the selection of matter, and in the various facts stated herein; in most cases I have personally verified them; great pains have also been exercised to exclude not only misleading, but also doubtful matter. I have no personal axe to grind whatever, nor am I connected either directly or indirectly with any firm of aeroplane builders, model or otherwise.

The statements contained in these pages are absolutely free from bias of any kind, and for them I am prepared to accept full responsibility.

I have to thank Messrs. A.W. Gamage (Holborn) for the use of various model parts for testing purposes, and also for the use of various electros from their modern Aviation Catalogue; also Messrs. T.W.K. Clarke & Co., of Kingston-on-Thames. For the further use of electros, and for permission to reproduce illustrations which have previously appeared in their papers, I must express my acknowledgment and thanks to the publishers of the "Model Engineer," "Flight," and the "Aero." Corrections and suggestions of any kind will be gratefully received, and duly acknowledged.

V.E. JOHNSON.


CONTENTS

INTRODUCTION.
  PAGE
§§ 1-5. The two classes of models—First requisite of a model aeroplane. § 6. An art in itself. § 7. The leading principle 1
CHAPTER I.
THE QUESTION OF WEIGHT.
§§ 1-2. Its primary importance both in rubber and power-driven models—Professor Langley's experiences. § 3. Theoretical aspect of the question. § 4. Means whereby more weight can be carried—How to obtain maximum strength with minimum weight. § 5. Heavy models versus light ones. 4
CHAPTER II.
THE QUESTION OF RESISTANCE.
§ 1. The chief function of a model in the medium in which it travels. § 2. Resistance considered as load percentage. § 3. How made up. § 4. The shape of minimum resistance. § 5. The case of rubber-driven models. § 6. The aerofoil surface—Shape and material as affecting this question. § 7. Skin friction—Its coefficient. § 8. Experimental proofs of its existence and importance. 7
CHAPTER III.
THE QUESTION OF BALANCE.
§ 1. Automatic stability essential in a flying model. § 2. Theoretical researches on this question. §§ 3-6. A brief summary of the chief conclusions arrived at—Remarks on and deductions from the same—Conditions for automatic stability. § 7. Theory and practice—Stringfellow—Pénaud—Tatin—The question of Fins—Clarke's models—Some further considerations. § 8. Longitudinal stability. § 9. Transverse stability. § 10. The dihedral angle. § 11. Different forms of the latter. § 12. The "upturned" tip. § 13. The most efficient section. 13
CHAPTER IV.
THE MOTIVE POWER.
Section I.—Rubber Motors.
§ 1. Some experiments with rubber cord. § 2. Its extension under various weights. § 3. The laws of elongation (stretching)—Permanent set. § 4. Effects of elongation on its volume. § 5. "Stretched-twisted" rubber cord—Torque experiments with rubber strands of varying length and number. § 6. Results

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