Hostname: page-component-cd9895bd7-dzt6s Total loading time: 0 Render date: 2024-12-26T17:47:17.632Z Has data issue: false hasContentIssue false
  • English
  • Français

Hypersonic missiles — some problem areas

Published online by Cambridge University Press:  04 July 2016

R. A. East  and
J. A. Edwards
R. A. East
Affiliation:
School of Engineering Sciences (Aeronautics and Astronautics) , University of Southampton , Southampton, UK
J. A. Edwards
Affiliation:
Weapons Systems Sector , DERA, Fort Halstead , Sevenoaks, UK
Get access Rights & Permissions [Opens in a new window]

Abstract

An overview of some of the problems, which have to be overcome in the design of hypersonic missiles or projectiles, is given. In the main, these are connected with the high levels of heat transfer rate suffered by such vehicles, particularly those induced by aerodynamic control surfaces. Some of the aspects of heat transfer, induced by, and suffered by such controls are presented. Data are presented and discussed, regarding the effects of flow separation due to flaps or flares, the effects of sharp and bluff fins (both swept and unswept). Finally, the aerodynamic interactions and heat transfer rates induced by reaction control jets are presented.

Type
Research Article
Information
The Aeronautical Journal , Volume 105 , Issue 1053 , November 2001 , pp. 643 - 651
Copyright
Copyright © Royal Aeronautical Society 2001 

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. J.D., Anderson Hypersonic and High Temperature Gas Dynamics, McGraw-Hill, 1989.Google Scholar
2. M.E., Tauber and G.P., Meneses Aerothermodynamics of transatmospheric vehicles. AIAA Paper No 86-1257, 1986.Google Scholar
3. G.T., Roberts and R.A., East Liquid crystal thermography for heat transfer measurement in hypersonic flows: a review, J Spacecraft and Rockets, 1996, 33, (6), pp 761–768.Google Scholar
4. D.A., Needham and J.L., Stollery Hypersonic studies of incipient separation and separated flows, AGARD conference proceedings number4. separated flows, part I. 1989.Google Scholar
5. G.S., Settles and L.J., Dodson Supersonic and hypersonic shock/boundary layer interaction database, AIAA J. 1994, 32, (7). pp 1377–1383.Google Scholar
6. A.J.D., Smith The Dynamic Response of a Wedge Separated Hypersonic Flow and its Effects on Heat Transfer, University of Southampton PhD Thesis. 1993.Google Scholar
7. H., Gortler Uber ein drcidimensionalc instability laminarer gren/shiehlen an konkaven wanden. Nachr Ges Wiss, Gottingen, Math PhysKI. I, pi, 1949; see also NACATM 1375.Google Scholar
8. A.J.D., Smith and R.A., East Unpublished work, 1992.Google Scholar
9. H., Bahinsky and J.A., Edwards On the incipient separation of a turbulent hypersonic boundary layer. Aeronaut J, 1996, 100. (996), pp 209–214.Google Scholar
10. J.A., Edwards and I.J., Roper Computational investigation of the incipient separation of a hypersonic turbulent boundary layer, AIAA Paper 97-0769, 1997.Google Scholar
11. Z.U., Haq Hypersonic Vehicle Interference Heating, University of Southampton PhD Thesis, 1993.Google Scholar
12. P.H., Schuricht Liquid Crystal Thermography in High Speed Flows, University of Southampton PhD Thesis, 1999.Google Scholar
13. J.L., Stollery, N.R., Fominson and S., Hussain The effects of sweep and bluntness on glancing interactions at supersonic speeds. ICAS Paper No 86-1.2.1., 1986.Google Scholar
14. B., Edney Anomalous heat transfer and pressure distributions on blunt bodies at hypersonic speeds in the presence of an impinging shock. FFA (Aeronautical Research Institute of Sweden) Report 115, 1968.Google Scholar
15. A.D., Dupuis and J.A., Edwards Free-flight tests, analysis and aero- heating aspects of two hypersonic configurations. 15th International Symposium on Ballistics. Jerusalem, 1995.Google Scholar
16. J.A., Edwards and A.D., Dupuis Flight tests of fin heating and ablation at Mach 5 and 6. AIAA Paper 00-0555, 2001.Google Scholar
17. D.I.A., Poll The effect of wing sweep back upon transition in hyper sonic flow, AIAA Paper 95-6090, 1995.Google Scholar
18. D.S., Dolling High speed turbulent separated flows: consistency of mathematical models and flow physics, AIAA .1, 1998, 36. (5), pp 725–732.Google Scholar
19. O.R., Tdtty, G.T., Roberts, R.A., East and W., Huntinoton-Thresher Numerical study of fin-body interference effects at hypersonic speeds. In Proceedings of the Second European Symposium on Aerothermodynamics for Space Vehicles, ESTEC, pp 51–56, 1995.Google Scholar
20. H.E.G., Powrie A Study of the Interaction Between an Underexpanded Normal Jet and a Hypersonic Free Stream, University of Southampton PhD Thesis, 1996.Google Scholar
21. J., Brandfis and J., Gill Experimental investigation of super- and hypersonic jet interaction on missile configurations, J Spacecraft and Rockets, 1998, 35, (3), pp 296–302.Google Scholar
22. J., Brandeis and J., Gill Experimental investigation of side-jet steering for supersonic and hypersonic missiles. J Spacecraft and Rockets. 1996. 33, (3), pp 346–352.Google Scholar
23. N.R., Mudford, G.T., Roberts, P.H., Schuricht, G.J., Ball and R.A., East Interference healing caused by a 3D transverse jet in hypersonic flow. Shock Waves (B., Sturtevant, J.E., Shepherd and H.G., Hornung (Eds)), 1995, 1. pp 173–178.Google Scholar
24. N., Qin and A., Redlich Massively separated flows due to transverse sonic jet in laminar hypersonic stream. Shock Waves. 1999, 9, pp 87–93.Google Scholar
25. D.M., Bushnell and L.M., Weinstein Correlation of peak heating for reattachment of separated flows, J Spacecraft and Rockets, 1968, 5. (9). pp 1111–1112.Google Scholar
26. F.T., Hung Interference heating due to shock wave impingement on laminar and turbulent boundary layers, AIAA Paper 7.3-678. 1973.Google Scholar
27. W.L., Hankey and M.S., Holden Two-dimensional shock wave- boundary layer interactions in high speed flows, AGARDograph 203. 1975.Google Scholar