Establishment of test conditions in the RHYFL-X facility
暂无分享,去创建一个
Peter A. Jacobs | Richard G. Morgan | K. J. Austin | B. S. Stewart | D. M. Jenkins | R. Morgan | P. Jacobs | D. Jenkins | K. Austin
[1] Peter A. Jacobs,et al. The RHYFL facility as a high performance expansion tube for scramjet testing , 2000 .
[2] John I. Erdos,et al. Facility opportunities and associated stream chemistry considerations for hypersonic air-breathing propulsion , 1994 .
[3] Peter A. Jacobs. MB_CNS: A Computer Program for the Simulation of Transient Compressible Flows , 1996 .
[4] Richard G. Morgan. Development of X3, A superorbital expansion tube , 2000 .
[5] W. R. Davies,et al. Heat transfer and transition to turbulence in the shock-induced boundary layer on a semi-infinite flat plate , 1969, Journal of Fluid Mechanics.
[6] Robert J Bakos. An investigation of test flow nonequilibrium effects on scramjet combustion , 1994 .
[7] R. J. Stalker,et al. Exporting Hypervelocity Technology , 1990 .