The RHYFL facility as a high performance expansion tube for scramjet testing
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[1] Robert J Bakos. An investigation of test flow nonequilibrium effects on scramjet combustion , 1994 .
[2] Richard G. Morgan. Development of X3, A superorbital expansion tube , 2000 .
[3] Con J. Doolan,et al. A two stage free-piston driver for expansion tubes , 1996 .
[4] Allan Paull,et al. Test flow disturbances in an expansion tube , 1992, Journal of Fluid Mechanics.
[5] Unmeel B. Mehta,et al. Strategy for developing air-breathing aerospace planes , 1996 .
[6] Robert L. Trimpi,et al. A Preliminary Theoretical Study of the Expansion Tube, a New Device for Producing High-Enthalpy Short-Duration Hypersonic Gas Flows , 1962 .
[7] Robert A Palmer. Measurement of heat transfer in superorbital flows , 2000 .
[8] Sudhir L. Gai. Free piston shock tunnels: developments and capabilities , 1992 .
[9] Richard G. Morgan,et al. Supersonic Hydrogen Combustion with a Short Thrust Nozzle , 1984 .