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Static and dynamic pitch stability of a blunted cone with forward facing aerodynamic spike in hypersonic flow

Published online by Cambridge University Press:  04 July 2016

G.R. Hutt  and
R.A. East
G.R. Hutt
Affiliation:
Department of Aeronautics and Astronautics, University of Southampton
R.A. East
Affiliation:
Department of Aeronautics and Astronautics, University of Southampton
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Extract

This paper presents experimental data highlighting the effects of a forward facing aerodynamic spike on the pitch stability of a blunted cone in hypersonic flow. Spike length and angle of attack variations on stability derivatives are described. Suitable application of the inviscid embedded Newtonian pitch stability prediction technique shows how the influence of spike aerodynamics may be successfully modelled. The paper extends the knowledge of aerodynamic spike flow effects, which have to date concentrated on aerodynamic drag reduction qualities at zero degrees angle of attack.

Type
Research Article
Information
The Aeronautical Journal , Volume 89 , Issue 888 , October 1985 , pp. 307 - 314
Copyright
Copyright © Royal Aeronautical Society 1985 

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References

1. Bogdonoff, S. M. and Vas, I. E. Preliminary investigations of spiked bodies at hypersonic speeds. J Aero / Space Sciences, 1959. 26,2.Google Scholar
2. Maull, D. J. Hypersonic flow over axially symmetric spiked bodies. J Fluid Mechanics, 1960, 8, Pt IV.Google Scholar
3. Wood, C. J. Hypersonic flow over spiked cones. J Fluid Mechanics, 1961,12, Pt IV.Google Scholar
4. Metcalfe, H. Some aspects of the design of hypersonic vehicles. Colston Papers, 1960.Google Scholar
5. East, R. A. and Qasrawi, A. M. S. A long stroke isentropic free piston hypersonic wind tunnel. ARC R&M No 3844,1978.Google Scholar
6. Hutt, G. R. and East, R. A. Optical techniques of model position measurement in dynamic wind tunnel testing. J Inst of Measurement and Control, 1985,18,3.Google Scholar
7. Khalid, M. A theoretical and experimental study of the hypersonic dynamic stability of blunt axi-symmetric conical and power law shaped bodies. PhD Thesis, University of Southampton, 1977.Google Scholar
8. East, R. A. Non-linear hypersonic static and dynamic stability of axi-symmetric shapes. Euromech Colloquium No 126, Berlin, 1980.Google Scholar
9. Ward, L. K. Influence of boundary layer transition on dynamic stability at hypersonic speeds. Paper No 6. Transactions of the 2nd technical workshop on dynamic stability testing. Arnold Air Force Station. Tenn. 1965.Google Scholar
10. Hutt, G. R. and East, R. A. Effects of large oscillation amplitude on axi-symmetric vehicle longitudinal static and dynamic stability in hypersonic flow. AIAA 83-0215,1983.Google Scholar
11. Ericsson, L. E. Hyperballistic Vehicle Dynamics. J Spacecraft and Rockets, 19,496–505,1982.Google Scholar
12. Seiff, A. Secondary flowfields embedded in hypersonic shock layers. NASA TND 1304,1962.Google Scholar
13. Ericsson, L. E. Unsteady embedded Newtonian flow. Astronautica Acta, 18, 309–330. 1973.Google Scholar
14. Ericsson, L. E. et al. Modifications of aerodynamic predictions of the longitudinal dynamics of tactical weapons. Lockheed Missile and Space Company Inc. LMSC D 646353,1979.Google Scholar
15. Calarese, W. Flow visualisation and data analysis of self-sustained shock oscillations on a spiked body at Mach 3. ICIASF Record 201-206,1981.Google Scholar
16. Reding, J. P., Guenther, R. A. and Richter, B. J. Unsteady Aerodynamic Considerations in the Design of Drag Reduction Spike. J Spacecraft and Rockets, 14,54–60,1977.Google Scholar