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Hypersonic flow over axially symmetric spiked bodies

Published online by Cambridge University Press:  28 March 2006

D. J. Maull
D. J. Maull
Affiliation:
Department of Aeronautics, Imperial College, London University
Now at Engineering Laboratory, University of Cambridge.
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Abstract

An investigation has been made of the flow over axisymmetric spiked bodies at a Mach number of 6·8. For some ranges of the ratio of spike length to body diameter the flow was found to be unsteady. The effect of the shape of the body nose on this unsteadiness was investigated and an explanation of the mechanism of the oscillation is given.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 8 , Issue 4 , August 1960 , pp. 584 - 592
Copyright
© 1960 Cambridge University Press

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References

Bogdonoff, S. M. & Vas, E. 1959 J. Aero./Space Sci. 26, 65.
Chapman, D. R., Kuehn, D. M. & Larson, H. K. 1957 NACA TN 3869.
Eggers, A. J. & Allen, M. J. 1958 NACA Rep. 1381.
Mair, W. A. 1952 Phil. Mag. 43, 695.
Moeckel, W. E. 1951a NACA TN 2418.
Moeckel, W. E. 1951b NACA RM E51 I25.
Stollery, J., Belcher, B. & Maull, D. J. 1960 J. R. Aero. Soc. 64, 24.