Hostname: page-component-77c89778f8-7drxs Total loading time: 0 Render date: 2024-07-17T06:14:29.376Z Has data issue: false hasContentIssue false
  • English
  • Français

Supersonic Jet Deflection

Published online by Cambridge University Press:  04 July 2016

R. P. Fraser  and
P. N. Rowe
R. P. Fraser
Affiliation:
Imperial College of Science and Technology, London
P. N. Rowe
Affiliation:
Imperial College of Science and Technology, London
Get access Rights & Permissions [Opens in a new window]

Extract

Appreciable forces can be obtained for steering a vehicle by the use of aerofoils whenever the relative air velocity is high and the air density is not too small. In practice this means velocities greater than 100 ft./sec. and altitudes below about 50,000 ft. Even when they are not in use for steering, aerofoils necessarily add to the drag of the vehicle.

Type
Research Article
Information
The Aeronautical Journal , Volume 62 , Issue 565 , January 1958 , pp. 43 - 59
Copyright
Copyright © Royal Aeronautical Society 1958

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1.Crow, A. D. (1948). The Rocket as a Weapon of War in the British Forces. Proceedings of the Institution of Mechanical Engineers, 158, 1948.CrossRefGoogle Scholar
2.Earring, W. G. A. (1946). A Critical Review of German Long Range Rocket Development. Journal of the Royal Aeronautical Society, Vol. 50, July 1946.Google Scholar
3.Seifert, H. S. (1955). Twenty-five Years of Rocket Development. Jet Propulsion, 25 (11), 1955.Google Scholar
4.Walter, H. (1954). Experience with the Application of Hydrogen Peroxide for the Production of Power. Jet Propulsion, 24 (3), 1954.Google Scholar
5.Felt, N. E. (1955). Development of a Stabilisation System for the Viking Rocket. Jet Propulsion, 25 (8), 1955.Google Scholar
6.Gardner, G. W. H. (1955). Guided Missiles. Proceedings of the Institution of Mechanical Engineers, 169, p. 30, 1955.CrossRefGoogle Scholar
7.Cunsolo, D. (1951). Calculation of the Shape of a Two-Dimensional Supersonic Nozzle in Closed Form. L'Aero-technica, 31, August 1951 (N.A.C.A. Translation, T.M.I358, January 1953).Google Scholar
8.Cleaver, A. V. (1951). Rockets and Assisted Take Off. Journal of the Royal Aeronautical Society, 55, Feb. 1951.Google Scholar
9.Burgess, E. (1953). Rocket Exploration of the Upper Atmosphere. Aircraft Engineering, 25, 1953.CrossRefGoogle Scholar
10.Kodosch, M. and De La Salle, L.De, J. (1954). Means of Controlling the Direction of a Stream of Ionised Fluid. Brit. Pat. Spec. 711,929. Completed 14th July, 1954.Google Scholar
11. Editorial Articles on Vertical Take Off. (1956). Interavia XI, No. 1, p. 19, January 1956.Google Scholar
12. Editorial Article on Vertical Take Off. (1955). Interavia X, No. 1, p. 27, January 1955.Google Scholar
13.Fraser, R. P., Rowe, P. N. and Coulter, M. O. (1957). The Efficiency of Supersonic Nozzles for Rockets and Some Unusual Designs. Proceedings of the Institution of Mechanical Engineers, 171, 1957.Google Scholar
14.Fraser, R. P. and Dombrowski, N. (1953). High Speed Photography in the Study of Moving Fluids. Proceedings of the Royal Photographic Society, Centenary Conference, London, 1953.Google Scholar
15.Eisenklam, P. (1953). Statistical Methods in Engineering Experimentation. Research, 6, 1953.Google Scholar
16.Thomson, J. J. and Thomson, G. P. (1928). The Conduction of Electricity through Gases. Cambridge University Press, 3rd. edition, p. 400, 1928.Google Scholar
17.Lewis, B. and Von Elbe, G. (1951). Combustion, Flames and Explosions of Gases. Academic Press Inc., p. 628 (Bibliography), 1951.Google Scholar
18.Keenan, J. G. (1946). Gas Turbines and Jet Propulsion. Oxford University Press, p. 142, 1946.Google Scholar
19.Stoney, G. G.et. al. (1923). Second Report of the Steam Nozzle Research Committee. Proceedings of the Institution of Mechanical Engineers, p. 311, March 1923.Google Scholar
20.Warren, G. B. and Keenan, J. H. (1926). A Machine for Testing Steam Turbine Nozzles by the Reaction Method. Transactions of the American Society of Mechanical Engineers, 48, p. 33, 1926.Google Scholar
21.Blackaby, J. R. (1951). An Investigation of the Effects of Jet-Outlet Cut-Off Angle on Thrust Direction and Body Pitching Moment. N.A.C.A. T.N. 2379, June 1951.Google Scholar
22.Bonney, E. A., Zucrow, M. J. and Besserer, C. W. (1956). Principles of Guided Missile Design, Vol. II. D. van Nostrand Co., 1956.Google Scholar
23.Rousso, M. D. and Baughman, L. E. (1956). Spreading Characteristics of a Jet Expanding from Choked Nozzles at Mach 191. N.A.C.A. T.N. 3836, December 1956.Google Scholar
24.Fraser, R. P. and Rowe, P. N. (1956). British Patent Application 25841/56, August 1956.Google Scholar