| N. Sahoo, D. R. Mahapatra, G. Jagadeesh, S. Gopalakrishnan, and K. P. J. Reddy. Design and analysis of a flat accelerometer-based force balance system for shock tunnel testing. Measurement: Journal of the International Measurement Confederation, 40(1): 93-106, 2007. | |
| V. Menezes, S. Saravanan, G. Jagadeesh, and K. P. J. Reddy. Experimental investigations of hypersonic flow over highly blunted cones with aerospikes. AIAA Journal, 41(10): 1955-1966, 2003. CrossRef | |
| R. Joarder, and G. Jagadeesh. A new free floating accelerometer balance system for force measurements in shock tunnels. Shock Waves, 13(5): 409-412, 2004. CrossRef | |
| J. D. Anderson Jr. Hypersonic and High Temperature Gas Dynamics 2nd Edition, AIAA Inc., Virginia, 2006. | |
| K. Tanimizu, D. J. Mee, R. J. Stalker, and P. A. Jacobs. Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: Theory and experiment. Shock Waves, 19(2): 83-93, 2009. CrossRef | |
| T. Mitani, T. Kanda, T. Hiraiwa, Y. Igarashi, and K. Nakahashi. Drags in scramjet engine testing: Experimental and computational fluid dynamics studies. Journal of Propulsion and Power, 15(4): 578-583, 1999. CrossRef |
Measurement of Drag on a Scramjet Engine in a Shock Tunnel
K. AnbuselvanRelated information
1 Department of Aerospace Engineering, Indian Institute of Technology Bombay, Powai, Mumbai 400076, INDIA
, V. MenezesRelated information1 Department of Aerospace Engineering, Indian Institute of Technology Bombay, Powai, Mumbai 400076, INDIA
, K. KumarRelated information1 Department of Aerospace Engineering, Indian Institute of Technology Bombay, Powai, Mumbai 400076, INDIA