A New Combustion-Driver 1.1 m Diameter Hypersonic Shock Tunnel to Simulate Mach 10 Flight Conditions

Author:

Minucci Marco A.1,Rego Israel1,Vilela Renan G.1,Fraile André C.1,Borges Marcos1,Santos Rafael1,Assunção Thiago1,Ponchio Camillo Giannino1,Galembeck Lucas1,Carinhana Jr. Dermeval1,Ribeiro Lucas A.1

Affiliation:

1. Institute for Advanced Studies

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. Gasdynamics Series;Lukasiewicz J.,1973

2. Richmond, J. K., Parsons, R. J. and Swithenbank, J. "On Shock-Tunnel Simulation of Scramjet Combustion Chamber Performance,"AIAAPaper 69-84, January 1969.

3. Bélanger, J. and Hornung, H. G. "A Combustion Driven Shock Tunnel to Complement the Free Piston Shock Tunnel T5 at GALCIT,"AIAA Paper 92-3968,July1992.

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