Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach numbers

Shock Waves

Volumn 12, Issue 3, 2002, Pages 197-204

  Menezes, Viren ^a   Saravanan, S ^a   Reddy, K P J ^a  

^a INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

Accelerometer force balance; Drag reduction; Hypersonic shock tunnel; Large angle blunt cone; Spike

Indexed keywords

EID: 0036877489     PISSN: 09381287     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00193-002-0160-3     Document Type: Article

References (21)

1. Anderson JD (1989) Hypersonic and high temperature gas dynamics. McGraw-Hill, New York
2. Bogdonoff SM, Vas IE (1959) Preliminary investigations of spiked bodies at hypersonic speeds. J Aer Sci 26:65
3. Crawford DH (1959) Investigation of the flow over a spiked-nose hemisphere-cylinder. NASA TN D-118
4. Gnemmi P, Srulijes J, Roussel K, Runne K (2001) Flow field around spike-tipped bodies. AIAA Paper 2001-2464
5. Huebner LD, Mitchell AM, Boudreaux EJ (1995) Experimental results on the feasibility of an aerospike for hypersonic missiles. AIAA Paper 95-0737
6. Hutt GR, Howe AJ (1989) Forward facing spike effects on bodies of different cross section in supersonic flow. The Aero J 93:229
7. Intrieri PF, Kirk DB (1987) High-speed aerodynamics of several blunt-cone configurations. J Spacecraft 24:127
8. Jagadeesh G, Dhinagaran R, Haridoss K, Reddy KPJ (1999) Convective heat transfer computations over large angle blunt cones using CFX-TASCFLOW. CFX Users' (Int.) Meeting at Friedrichshafen, Germany
9. Khabiry SL, Colver GM (1997) Drag reduction by dc corona discharge along an electrically conductive flat plate for small Reynolds number flow. Phys Fluids 9:587
10. Marsh JJ, Myrabo LN, Messitt DG, Nagamatsu HT (1996) Experimental investigation of hypersonic "Air Spike" inlet at Mach 10. AIAA Paper 96-0721
11. Maull DJ (1960) Hypersonic flow over axially symmetric spiked bodies. J Fluid Mech 8:584
12. McMahon HM (1959) An experimental study of the effect of mass ejection at the stagnation point of a blunt body. Memo. No.42, Hypersonic Res. Project, GALCIT
13. Meyer BM, Nelson HF, Riggins DW (2001) Hypersonic drag and heat-transfer reduction using a forward-facing jet. J Aircraft 38:680
14. Minucci MAS, Bracken RM, Myrabo LN, Nagamatsu HT, Shanahan KJ (2000) Experimental investigation of an electric arc simulated "Air spike" in hypersonic flow. AIAA Paper 00-0715
15. th Int. Symp. on Shock Waves, pp 358
16. Reddy NM, Nagashetty K, Jagadeesh G, Reddy KPJ (1996) Review of research investigations during 1975-1995 in IISc hypersonic shock tunnel (HST1) at hypersonic Mach numbers. Sadhana-Proc Ind Aca of Sci 21:741
17. Reding JP, Guenther RA, Richter BJ (1977) Unsteady aero-dynamic considerations in the design of a drag-reduction spike. J Spacecraft 14:54
18. Riggins DW, Nelson HF, Johnson E (1999) Blunt body wave drag reduction using focused energy deposition. AIAA J 37:460
19. nd Int Symp Space Tech and Sci Japan, ISTS 2000-e-23
20. Thurman WE (1964) A flow-separation spike for hypersonic control of a hemisphere-cylinder. AIAA J 2:159
21. Wood CJ (1961) Hypersonic flow over spiked cones. J Fluid Mech 12: 614