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Naval Architecture in Aeronautics
Published online by Cambridge University Press: 14 September 2016
Abstract
- Type
- Proceedings
- Information
- Copyright
- Copyright © Royal Aeronautical Society 1920
References
Note on page 324 (1) Bouguer, “ Traité du navire,” Paris, 1746.
L. Euler, “ Scientia Navalis,” St. Petersburg, 1749.
Atwood, “ Stability of Ships,” London, 1796.
Chas. Dupin, “ Applications de Géometrie et de mecanique à la Marine,” Paris, 1822.
P. J. Moreau, “ Principes fondamentaux de l'equilibre,” etc., Lorient, 1830.
J. M. C. Duhamel, La stabilité des corps flottants,” Paris, 1832.
H. Moseley, “ On the Dynamical Stability and on the Oscillations of Floating Bodies,” London, 1874.
F. K. Barnes, “ On the Metacentre and Metacentric Curves,” “ Naval Science,” Vol. III., London, 1850.
E. J. Reed, “ A Treatise on the Stability of Ships,” London, 1885.
Note on page 325 (1) D. Bernoulli (Prix de 1'Academie des sciences), Paris* 1757.
Dupuy de Lôme, “ Mem. G.M.,” Vol. IV., Paris, 1859.
Wm. Froude, “ Proc. Inst. Nav. Arch.,” Vols. II., III., IV., XIV., XVI., London.
Rankinc, “Proc. Inst. Nav. Arch.,” Vols. V., XII., London.
Scott Russcl, “ Proc. Inst. Nav. Arch.,” Vol. IV., London.
Bertin, “ Les vagucs et le roulis,” Berger-Levraut, Paris, 1877.
Reech, “ Thérie du roulis, etc.,” Paris, 1870.
Note on page 325 (2) Bryan, G. H., “Stability in Aviation,” Macmillan, London, 1911 Google Scholar.
Note on page 325 (3) L. Bairstow, Advisory Committee for Aeronautics, R. & M., 116—122, London, 1914.
Note on page 326 (1) A positive value of Mw in Bairstow's notation.
Note on page 326 (2) Hunsaker, “Dynamical Stability of Aeroplanes,” Smithsonian Misc. Coll., Vol. LXII, No. 5.
Note on page 332 (1) Leclert, “ Naval Science,” April—October, 1872.
Note on page 335 * I am indebted to my assistant, Lieut. R. D. MacCart, for help in the preparation of this Appendix.
Note on page 367 * I am indebted to my assistant, R. B. Beisel, B.S., for help in the preparation of this Appendix.
Note on page 377 (1) “ Stabiliser and Elevator Pressure Distribution,” Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A., Vol. II., No. 3, December, 1918.
Note on page 379 (2) “ Airplane Control Surfaces,” J. C. Hunsaker and T. H. Huff, “ Aviation,” Vol. I., No. 5, . October 1, 1916.
Note on page 380 (1) Formules Approximatives de Construction Navale, Paris, 1870.
Etude sur les Torpilleurs (translation), Office of Naval Intelligence, U.S., General Information Series, Washington, 1886.
The Displacement and Dimensions of Ships, Int.Eng. Congress, Glasgow, 1901.
Note on page 380 (2) I am indebted to Mr. C. P. Burgess for assistance in applying Normand's equation to airships, and I have also had access to Professor Hovgaard's manuscript for his forthcoming book, “ General Design of Warships,” Spon, London.
Note on page 383 (1) Proof of this formula seems unnecessary. A somewhat similar form has been shown by Cole, “ Aeronautical Journal,” March, 1920, and by Campbell, Inst. of Nav. Arch., March 25, 1920. The exact form here used applies to the case of uniform lateral load on a wire initially just taut.
Note on page 384 (1) There is some reason to believe that r is increased for L/D below 5.5 and above 8.5. For the usual range of ship forms the change is small and rather uncertain.
Note on page 385 (1) A. P. Cole, Aeronautical Journal, p. 118, March, 1920.
Note on Page 393 (1) W. Hovgaard, “ General Design of Warships,” Spon, London, 1920.
Note on Page 393 (2) C. R. Campbell, “ Inst. Nav. Arch.,” London, March, 1920.
Note on Page 393 * I am indebted to my assistant, Lieut. C. B. Harper, for help in the preparation of this Appendix.
Note on Page 399 (1) H. C. Richardson, Society Naval Architects and Marine Engineers, New York, Nov., 1916.
G. S. Baker, “ Flying Boats,” etc., North-East Coast Institution of Engineers and Shipbuilders, Newcastle, Februarv 27, 1920.
Note on Page 405 (1) Advisory Committee for Aeronautics, R. & M. 469.
Note on Page 405 (2) A. F. Zahm, “ Journal of the Franklin Institute,” Philadelphia, August, 1919.
Note on Page 405 (3) G. S. Baker, Advisory Committee for Aeronautics, R. & M. 583.