Counterflow drag reduction by supersonic jet for a blunt body in hypersonic flow

Physics of Fluids

Volumn 18, Issue 11, 2006, Pages

  Venukumar, Balla ^a   Jagadeesh, G ^a   Reddy, K P J ^a  

^a INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; FLOW VISUALIZATION; JETS; MATHEMATICAL MODELS; SCHLIEREN SYSTEMS; SHOCK TUBES; SUPERSONIC AERODYNAMICS;

ACCELOREMETER BASED FORCE BALANCE SYSTEM; DRAG COEFFICIENT; MACH NUMBER; SUPERSONIC JET;

HYPERSONIC FLOW;

DRAG; FLOW VISUALIZATION; HYPERSONIC FLOW; JETS; MATHEMATICAL MODELS; SCHLIEREN SYSTEMS; SHOCK TUBES; SUPERSONIC AERODYNAMICS;

EID: 33751585005     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.2401623     Document Type: Article

References (9)

1. R. J. Stalker, A. Paull, D. J. Mee, R. G. Morgan, and P. A. Jacobs, "Scramjets and shock tunnels-The Queensland experience," Prog. Aerosp. Sci.PAESD60376-0421 41, 471 (2005).
2. V. Menezes, S. Saravanan, and K. P. J. Reddy, "Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach numbers," Shock WavesSHWAEN0938-128710.1007/s00193-002-0160-3 12, 197 (2002).
3. Niranjan Sahoo, Vinayak Kulkarni, S. Saravanan, G. Jagadeesh, and K. P. J. Reddy, "Film cooling effectiveness on a large angle blunt cone flying at hypersonic speed," Phys. FluidsPHFLE61070-663110.1063/ 1.1862261 17, 036102 (2005).
4. V. Menezes, S. Kumar Maruta, K. P. J. Reddy, and K. Takayama, "Hypersonic flow over a multi-step afterbody," Shock WavesSHWAEN0938-128710.1007/s00193-005-0281-6 14, 421 (2005).
5. K. Nagashetty, K. Syed Saifuddin, S. Saravanan, K. S. Gurumurthy, G. Jagadeesh, and K. P. J. Reddy, "Visualization of shock shapes around blunt bodies at hypersonic Mach number in a shock tunnel using electrical discharge technique," Curr. Sci.CUSCAM0011-3891 79, 1086 (2000).
6. Niranjan Sahoo, Kiran Suryavamshi, K. P. J. Reddy, and David J. Mee, "Dynamic force balances for short duration hypersonic testing facilities," Exp. FluidsEXFLDU0723-486410.1007/s00348-005-0932-5 38, 606 (2005).
7. Niranjan Sahoo, D. R. Mahapatra, G. Jagadeesh, S. Gopalakrishnan, and K. P. J. Reddy, "An accelerometer balance system for measurement of aerodynamic force coefficients over blunt bodies in a hypersonic shock tunnel," Meas. Sci. Technol.MSTCEP0957-023310.1088/0957-0233/14/3/ 303 14, 260 (2003); (http://stacks.iop.org/MST/14/260).
8. E. Josyula, M. Pinney, and W. B. Blake, "Application of a counterflow drag reduction technique in high speed systems," AIAA Paper 01-2437.
9. Kentaro Hayashi and Shigeru Asoy, "Effect of pressure ratio on aerodynamic heating reduction due to opposing jet," AIAA Paper 03-4041.