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The United Kingdom's contributions to the development of aeronautics: Part 2. The development of the practical aeroplane (1900-1920)

Published online by Cambridge University Press:  04 July 2016

J. A. D. Ackroyd
J. A. D. Ackroyd*
Affiliation:
Aerospace Division, Manchester School of Engineering, University of Manchester, Manchester, UK
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Extract

The first part of this survey dealt mainly with the development of the earliest ideas on air resistance and their application to flight. That part of the survey paused at the achievement of powered flight during the early years of the twentieth century. Even then, the main problem remained as that of aerodynamics, a subject only vaguely understood by those aviation pioneers endeavouring to get off the ground. For them theoretical guidelines, as yet, could offer little help. One of the earliest of those very few analytically based results to achieve general acceptance was the statement that resistance is proportional to the product of fluid density, a characteristic body area and the square of the flow's speed. This result had appeared during the seventeenth century in Newton's work and had received some experimental confirmation. Newton's concurrent ‘rare medium’ concept, viewing fluid flow as a stream of disconnected particles, gained credence at that time since its results agreed with the above resistance proportionality. Yet this concept became mistakenly applied to airflow so as to predict plate resistances proportional to the square of the sine of the plates' incidence angles, a misleading result which caused confusion for at least the next century.

Type
Research Article
Information
The Aeronautical Journal , Volume 104 , Issue 1042 , December 2000 , pp. 569 - 596
Copyright
Copyright © Royal Aeronautical Society 2000 

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References

1. Ackroyd, J.A.D. The United Kingdom's contributions to the development of aeronautics; Part 1. From antiquity to the era of the Wrights, Aeronaut J, January 2000, 104, (1031), pp 9–30.Google Scholar
2. Kutta, M.W. Auftriebskräfte in strömenden Flüssigkeiten, Illus Aeronautische Mitteilungen, 1902, 6, pp 133–135.Google Scholar
3. Lilienthal, O. Der Vogelflug als Grundlage der Fliegekunst, Gaertners, Berlin, 1889. [Isenthal, A.W. (Trans.) Birdflight as the Basis of Aviation, Longmans Green & Co, London, 1911.]Google Scholar
4. Zhukovskii, N.E. On annexed vortices (in Russian), Trans Physical Section of the Imperial Society of the Friends of Natural Science, Moscow, 1906,13, pp 12–25.Google Scholar
5. Zhukovskii, N.E. De la chute dans l'air de corps léers de forme allongée, animés d'un mouvement rotatoire, Bulletin de l'Institute Aerodynamique de Koutchino, 1906,1, pp 51–65.Google Scholar
6. Kutta, M.W. Über eine mit den Grundlagen des Flugsproblems in Beziehung stehende zweidimensionale Strömung, Sitzungsberichte der königlich Bayerischen Akademie der Wissenschaften, 1910, 40, pp 1–58.Google Scholar
7. Chaplygin, S.A. On the pressure exerted by a plane-parallel flow on obstructing bodies (Aeroplane theory) (in Russian), Mathematical Collections of Moscow, 1910, 28, pp 120–166.Google Scholar
8. Zhukovskii, N.E. Über die Konturen der Tragflächen der Drachenflieger, Zeit für Flugtechnik und Motorluftschiffahrt, 1910, 1, pp 281– 284.Google Scholar
9. Zhukovskii, N.E. The Theoretical Basis of Aeronautics (in Russian), Moscow, 1912.Google Scholar
10. Betz, A. Untersuchung einer Joukowskyschen Tragfläche, Zeit für Flugtechnik und Motorluftschiffahrt, 1915, 6, pp 173–179.Google Scholar
11. Helmholtz, H.L.F. Von Über Intergrale der Hydrodynamischen Gleichungen, Welche den Wirbelbewegung Entsprechen, J für die Reine und Angew Math, 1858, 55, pp 25–55.Google Scholar
12. Giacomelli, R. and Pistolesi, E. Division D, Historical Sketch (Aerodynamic Theory, Vol 1, Durand, W.F. (Ed)), Springer Verlag, Berlin, 1934.Google Scholar
13. Prandtl, L. Tragflügeltheorie, I. Mitteilungen, Nach der kgl Gesellschaft der Wiss zu Göttingen, Math-Phys Klasse, 1918, pp 451–477.Google Scholar
14. Prandtl, L. Tragflügeltheorie, II Mitteilungen, Nach der kgl Gesellschaft der Wiss zu Göttingen, Math-Phys Klasse, 1919, pp 107– 137.Google Scholar
15. Glauert, H. The Elements of Aerofoil and Airscrew Theory, Cambridge University Press, 1926.Google Scholar
16. Prandtl, L. Über Flüssigkeitsbewegung bei sehr kleiner Reibung, Verhandlungen des dritten internationalen Mathematiker-Kongresses, Heidelberg, 1904, pp 489–491, Leipzig.Google Scholar
17. Blasius, P.R.H. Grenzschichten in Flüssigkeiten mit kleiner Reibung, Zeit für Mathematik und Physik, 1908, 56, pp 1–37.Google Scholar
18. Hiemenz, K. Die Grenzschicht an einem in den gleichförmigen Flüssigkeitsstrom eingetauchten geraden Kreiszylinder, Dinglers Polytech J, 1911, 326, pp 321–324, 344-348, 357-362, 372-376, 391-393, 407- 410.Google Scholar
19. Prandtl, L. Der Luftwiderstand von Kugeln, Nach der kgl. Gesellschaft der Wiss zu Göttingen, Math-Phys Klasse, 1914, pp 177– 190.Google Scholar
20. Finsterwalder, S. Die Aerodynamik als Grundlage der Luftschiffahrt, Zeit für Flugtechnik und Motorluftschiffahrt, 1910, 1, pp 6–10, 30-31.Google Scholar
21. Prandtl, L. The generation of vortices in fluids of small viscosity, JRAeS, 1927, 31, pp 718–741.Google Scholar
22. Routh, E.J. A Treatise on the Dynamics of the System of Rigid Bodies, London, 1860.Google Scholar
23. Bryan, G. H. and Williams, W. E. The longitudinal stability of aerial gliders, Proc Royal Soc A, 1904, 73, pp 100–116.Google Scholar
24. Bryan, G. H. Stability in Aviation, Macmillan, London, 1911.Google Scholar
25. Kingsford, P.W. F.W. Lanchester: A life of an engineer, Arnold, London, 1960.Google Scholar
26. Lanchester, F.W. Aerodynamics, Constable, London, 1907.Google Scholar
27. Ackroyd, J.A.D. Lanchester — The Man (The 31st Lanchester lecture), Aeronaut J, April 1992, 96, (954), pp 119–140.Google Scholar
28. Ackroyd, J.A.D. Lanchester's Aerodynamics (Chapter 5, The Lanchester Legacy, Vol III, Fletcher, J. (Ed)), Coventry University Press, 1996.Google Scholar
29. Lanchester, F.W. Improvements in and relating to aerial machines, 1897, Patent Specification No 3608, HMSO, London.Google Scholar
30. Rankine, W.J.M. On the mechanical principles of the action of propellers, Trans Inst Naval Arch, 1865, 6, pp 13–39.Google Scholar
31. Froude, W. On the elementary relation between pitch, slip and propulsive efficiency, Trans Inst Naval Arch, 1878, 19, pp 47–57.Google Scholar
32. Lanchester, F.W. The flying machine: the aerofoil in the light of theory and experiment, Proc Inst Auto Eng, 1915, 9, pp 171–259.Google Scholar
33. Lanchester, F.W. The part played by skin friction in aeronautics, JRAeS, 1937, 41, pp 68–131, 322-323.Google Scholar
34. Reynolds, O. An experimental investigation of the circumstances which determine whether the motion of water shall be direct or sinuous and of the law of resistance in parallel channels, Phil Trans Roy Soc A, 1883,174, pp 933–982.Google Scholar
35. Beaufoy, M. Nautical and Hydraulic Experiments, with Numerous Scientific Miscellanies, London, 1834.Google Scholar
36. Froude, W. Report to the Lords Commissioners of the Admiralty on Experiments for the Determination of the Frictional Resistance of Water on a Surface, under Various Conditions, Performed at Chelston Cross, under the Authority of Their Lordships, 44th Report of the British Association for the Advancement of Science, 1874, pp 249-255.Google Scholar
37. Lanchester, F.W. Aerofoils of high aspect ratio, ACA, R&M No 109, 1913.Google Scholar
38. Drzewiecki, S. Des hélices aériennes; Théorie générale des propulseurs hélicoidaux, et méthode de calcul de ces propulseurs pour l'air, Paris, 1909.Google Scholar
39. Lanchester, F.W. The screw propeller, Proc Inst Auto Eng, 1915, 9, pp 263–354.Google Scholar
40. Ackroyd, J.A.D. Lanchester's Review of Aeroplane Design and Construction (Chapter 7, The Lanchester Legacy, Vol III, Fletcher, J. (Ed)), Coventry University Press, 1996.Google Scholar
41. Lanchester, F.W. Aerodonetics, Constable, London, 1908.Google Scholar
42. Ackroyd, J.A.D. Lanchester's Aerodonetics (Chapter 6, The Lanchester Legacy, Vol III, Fletcher, J. (Ed)), Coventry University Press, 1996.Google Scholar
43. MacFarland, M.W. (Ed), The Papers of Wilbur and Orville Wright, Vols I and II McGraw-Hill, New York, 1953.Google Scholar
44. Walker, P.B. Early Aviation at Farnborough, Vols I and II, Macdonald, London, 1971.Google Scholar
45. Jarrett, P. Cody and his aeroplanes. Samuel Franklin Cody: his life and times, Air Enthusiast, 1999, (82), pp 6–17.Google Scholar
46. Gollin, A. No Longer an Island; Britain and the Wright brothers, 1902-1909, Heinemann, London, 1984.Google Scholar
47. Prins, F. ‘AV ’ His life and times; a biography of A.V. Roe, first Briton to fly and founder of a dynasty, Air Enthusiast, 1999, (81), pp 56–63.Google Scholar
48. Driver, H. The Birth of Military Aviation; Britain, 1903-1914, Royal Historical Society/Boydell Press, Suffolk, 1997.Google Scholar
49. Lanchester, F.W. Notes on the resistance of planes in normal and tangential presentation and on the resistance of ichthyoid bodies, ACA, R&M No 15, Part 1, 1909.Google Scholar
50. Zahm, A.F. Atmospheric friction of even surfaces, Phil Mag Ser 6, 1904, 8, pp 58–66 (See Appendix by Rayleigh).Google Scholar
51. Lord, Rayleigh Note as to the application of the principle of dynamic similarity, ACA, R&M No 15, Part 2, 1909.Google Scholar
52. Stanton, T.E. Report on the experimental equipment of the Aeronautical Department of the National Physical Laboratory, ACA, R&M No 25, 1910.Google Scholar
53. Jones, B.M. The resistance of wires and ropes in a uniform current of air, AC A, R&M No 40, Part 1, 1911.Google Scholar
54. Bairstow, L. and Jones, B.M. Experiments on model wings, ACA, R&M No 60, 1912.Google Scholar
55. Fage, A. and Cowley, W.L. Experiments on the variation of the forces and moments on an aerofoil as the speed changes; Part (it), Experiments on the variation of the position of the centre of pressure of an aerofoil as the speed changes, at small angles of incidence, ACA, R&M No 148, 1915.Google Scholar
56. Lanchester, F.W. The flying machine from an engineering standpoint, Proc Inst Civil Eng, 1914, 98, pp 3–96.Google Scholar
57. Bairstow, L., Jones, B.M. and Thompson, A.W.H. Investigation into the stability of an aeroplane, with an examination into the conditions necessary in order that the symmetric and asymmetric oscillations can be considered independently, ACA, R&M No 77, 1913.Google Scholar
58. Bairstow, L. and MacLachlan, L. A. The experimental determination of rotary coefficients, ACA, R & M No. 78, 1913.Google Scholar
59. Bairstow, L. An examination into the longitudinal stability of a monoplane of Bleriot type, based on the data furnished by model experiments. Discussion of lateral stability, in connection with experiments on the same monoplane model, ACA, R&M No. 79, 1913.Google Scholar
60. Bairstow, L., Nayler, J.L. and Jones, R. Investigation of the stability of an aeroplane when in circling flight, ACA, R&M No 154, 1914.Google Scholar
61. Bairstow, L., Hyde, J.H. and Booth, H. The new four-foot wind channel; with a description of the weighing mechanism employed in the determination of forces and moments, ACA, R&M No 68, 1913.Google Scholar
62. Bramwell, F.H., Relf, E.F. and Fage, A. On a determination on the whirling arm of the pressure-velocity constant for a Pitot (velocity head and static pressure) tube; and on the absolute measurement of velocity in aeronautical work, ACA, R&M No 71, 1912.Google Scholar
63. Fage, A. and Stern, W.J. Determination of the pressure distribution over the surface of a dirigible of Parseval form when oblique to the wind and comparison of the results with those obtained from total force measurements. Variation of head resistance of a dirigible of Parseval form with change of speed, ACA, R&M No 107, 1914.Google Scholar
64. Various Authors Experiments on models of aeroplane wings, ACA, R&M No 152, 1914.Google Scholar
65. Bairstow, L. and MacLachlan, L. A. A preliminary note on methods of calculation which may be employed in the determination of the stresses in the spars of aeroplane wings, ACA, R&M No 83, 1913.Google Scholar
66. Clapeyron, B.P.E. Calcul d'une poutre élastique reposant librement sur des appuis inégalement espacés, Comptes Rendus, 1857, 45, pp 1076–1080.Google Scholar
67. Clarke, T.W.K. Maximum loading attainable on the wings of an aeroplane owing to flattening out after a prolonged dive, ACA, R&M No 128, 1914.Google Scholar
68. Bairstow, L. and Stedman, E.W. The design of a strut of uniform strength, ACA, R&M No 158, 1914.Google Scholar
69. Barr, G. and Thomas, J. Experiments on aeroplane fabrics, ACA, R&M No 90, 1913.Google Scholar
70. Barr, G. Effect of various factors on the results obtained in the simple tensile test on linen fabric, ACA, R&M No 172, 1914.Google Scholar
71. Rosenhain, W. Report on light alloys, ACA, R&M No 91, 1913.Google Scholar
72. Lanchester, F.W. Report on high altitude flying and the development and improvement of the aeronautical motor, ACA, R&M No 220, 1915.Google Scholar
73. Clark, C.S. The Lanchester Legacy, Vol I, 1895-1931, Coventry University Press, 1995.Google Scholar
74. Lanchester, F.W. Surface cooling and skin friction, ACA, R&M No 94, 1913.Google Scholar
75. Reynolds, O. On the extent and action of the heating surface for steam boilers, Proc Manchester Lit Phil Soc, 1874, 14, pp 7-12.Google Scholar
76. Lanchester, F.W. Torsional vibrations of the tail of an aeroplane, ACA, R&M No 276, Part (i), 1916.Google Scholar
77. Bairstow, L. and Fage, A. Torsional vibrations of the tail of an aeroplane, ACA, R&M No 276, Part (ii), 1916.Google Scholar
78. Garrick, I.E. and Reed, W.H. Historical development of aircraft flutter, JAircr, 1981, 18, pp 897–912.Google Scholar
79. Lanchester, F.W. Aircraft in Warfare: the Dawn of the Fourth Arm, Constable, London, 1916.Google Scholar
80. Hobson, B.D. Aircraft at War: Strategy, Tactics and Related Topics (Chapter 8, The Lanchester Legacy, Vol III, Fletcher, J. (Ed)), Coventry University Press, 1996.Google Scholar
81. Bowen, K.C. and McNaught, K.R. Mathematics in Warfare: Lanchester Theory (Chapter 9, The Lanchester Legacy, Vol III, Fletcher, J. (Ed)), Coventry University Press, 1996.Google Scholar
82. Taylor, G.I. Pressure distribution round a cylinder, ACA, R&M No 191, 1916.Google Scholar
83. Taylor, G.I. Skin friction on a flat surface, ACA, R&M No 604, 1918.Google Scholar
84. Karman, T. Von Über laminare und turbulente Reibung, Zeit fär angew Mathematik und Mechanik, 1921,1, pp 233–252.Google Scholar
85. Taylor, G.I. Pressure distribution over the wing of an aeroplane in flight, ACA, R&M No 287, 1916.Google Scholar
86. Taylor, G.I. and Griffith, A.A. The use of the soap film in solving torsion problems, ACA, R&M No 333, 1917.Google Scholar
87. O'Gorman, M. Report on the precautions taken as to the strength of details on the B.E. class of aeroplanes; with Appendices, ACA R&M No 127, 1914.Google Scholar
88. Douglas, W.D. and Clegg, A.W. Methods employed at the Royal Aircraft Establishment for the experimental determination of the ultimate strength of aeroplane structures, ACA, R&M No 476, 1918.Google Scholar
89. Irving, H.B. Report on the strength of the wings of captured German aeroplanes, ACA, R&M No 350, 1917.Google Scholar
90. Cowley, W. L. and Levy, H. Critical loading of struts and structures, ACA R&M Nos 364, 1917; 373, 1918; 453, 1918; 484, 1918; 485, 1918; 566, 1918.Google Scholar
91. Southwell, R.V. On the determination of the stresses in braced frameworks; Part I, The effect of axial loading, flexure and torsion upon a framework of uniform rectangular cross-section, ARC R&M No 737, 1921; Part II, The effect of shear upon a framework of uniform rectangular cross-section, ARC R&M No 790, 1922; Part III, The effect of axial loading, torsion, flexure and shear upon a braced framework of any uniform cross-section, ARC R&M No 791, 1922; Part IV, The effect of axial loading, flexure, torsion and shear upon a tubular framework with taper, ARC, R&M No 819, 1922.Google Scholar
92. Relf, E.F. An empirical method for the prediction of wing characteristics from model tests, ACA, R&M No 450, 1918.Google Scholar
93. JRAeS, 1966, 70, Centenary Journal.Google Scholar
94. Irving, H.B. and Ower, E. Comparative tests of a biplane of RAF 15 wing section when fitted with wing tips of four different types, ACA, R&M No 557, 1918.Google Scholar
95. Various Authors Experiments on aerofoils, ACA, R&M No 195, 1916.Google Scholar
96. Pannell, J.R. and Jones, R. The design of a sensitive yawmeter, ACA, R&M No 445, 1918.Google Scholar
97. Fage, A. A description of a hot-wire anemometer which is sensitive over a large range of wind speed, ACA, R&M No 556, 1918.Google Scholar
98. King, L.V. On the convection of heat from small cylinders in a stream of fluid: determination of the convection constants of small platinum wires with applications to hot-wire anemometry, Phil Trans Roy Soc A, 1914,214, pp 375–432.Google Scholar
99. Lindemann, F.A. Turn indicators for aeroplanes, ACA, R&M No 525, 1917.Google Scholar
100. Lindemann, F.A.and Searle, G.F.C. Measurements of accelerations in flight, ACA, R&M No 376, 1917.Google Scholar
101. Lindemann, F.A. Glauert, H. and Harris, R.G. The experimental and mathematical investigation of spinning, ACA, R&M No 411, 1918.Google Scholar
102. Report of the Scale Effect Sub-Committee on the relation between model tests and the full scale performance of aeroplanes, ACA R&M No 374, 1917.Google Scholar
103. Bryant, L.W. and Batson, A.S. Test of the Fokker thick aerofoil section, ACA, R&M No 654, 1919.Google Scholar
104. Glauert, H. and Gates, S.B. Prediction of the performance and longitudinal stability of an aeroplane, including the estimation of the effect of small changes in the design, ACA, R&M No 324, 1917.Google Scholar
105. Glauert, H. The longitudinal control of an aeroplane, ACA, R&M No 470, 1918.Google Scholar
106. Gates, S.B. Control as a criterion of longitudinal stability, ACA, R&M No 636, 1919.Google Scholar
107. Glauert, H. The longitudinal stability of an aeroplane, ACA, R&M No 638, 1919.Google Scholar
108. Glauert, H. Aerofoil theory, ARC, R&M No 723, 1921.Google Scholar
109. Glauert, H. An aerodynamic theory of the airscrew, ARC, R&M No 786, 1922.Google Scholar
110. Prandtl, L. Applications of modern hydrodynamics to aeronautics, NACA,TR 116, 1921.Google Scholar
111. Stokes, P. Power for flight in the Victorian era, Aerospace, 1984, 11, (10), pp 10–18.Google Scholar
112. Tuck, W.J. Rotary engines, Aerospace, 1983, 10, (3), pp 12–19.Google Scholar
113. Gunston, W.T. The Development of Piston Aero Engines, Second Edition, Patrick Stephens, Somerset, 1999.Google Scholar
114. Gibbs-Smith, C.H. Aviation, an Historical Survey, Second Edition, HMSO, London, 1985.Google Scholar
115. Penrose, H. British Aviation, the Pioneer Years, Putnam, London, 1967.Google Scholar
116. Penrose, H. British Aviation, the Great War and Armistice, Putnam. London, 1969.Google Scholar
117. O'Gorman, M. Experiments with full-scale flying machines, ACA, R&M No 59, 1911.Google Scholar
118. O'Gorman, M. Report on full scale work, ACA, R&M No 86, 1913.Google Scholar
119. O'Gorman, M. Lateral stability, ACA, R&M No 133, 1914.Google Scholar
120. O'Gorman, M. and Mayo, R.H. Longitudinal stability, ACA, R&M No 134, 1914.Google Scholar
121. Loftin, L. Quest for performance. The evolution of modern aircraft, NASA SP 468, NASA, Washington DC, 1985.Google Scholar
122. Bruce, J.M. The Aeroplanes of the Royal Flying Corps (Military Wing), Putnam, London, 1982.Google Scholar
123. Abzug, M. J. and Larrabee, E.E. Airplane Stability and Control: A History of the Technologies that Made Aviation Possible, Cambridge University Press, 1997.Google Scholar
124. Penrose, H. Architect of Wings; A Biography of Roy Chadwick — Designer of the Lancaster Bomber, Airlife, Shrewsbury, 1985.Google Scholar
125. Tredrey, F.D. Pioneer Pilot; The Great Smith Barry who Taught the World how to Fly, Purnell, Oxon, 1976.Google Scholar