Computation and analysis of cross jet interaction flowfields of a biconic body at incidences
Author:
Affiliation:
1. U.S. Navy, Naval Surface Warfare Center, Dahlgren, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2625
Reference26 articles.
1. Secondary injection of gases into a supersonic flow
2. Prats,B.D.,Hill, J.A.F, Metzger,M.A.,and Harvey,D.W. "High AltitudeManeuverControlTests intheNSWCHypervelocityWindTunnel,"AIAA Paper 84-0616,March 1984.
3. Yeneriz,M.A.,DavisJ.R., Cooper, O.K.,and Harvey,D.W. "ComparisonofCalculationand ExperimentforaLateralJetfrom aHypersonicBiconic Vehicle,"AIAAPaper 89-2548, July 1989.
4. Interaction of jet in hypersonic cross stream
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