Design and testing of 2-D fixed-geometry hypersonic intakes
Author:
Affiliation:
1. Daimler-Benz Aerospace AG, Munich, Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1529
Reference18 articles.
1. T.M.Berens,N.C.Bissinger Forebody PrecompressionPerformance of HypersonicFlightTest Vehicles AIAA-98-1574,1998
2. N.C.Bissinger,D.M.Schmitz Design andTesting of 2-D HypersonicIntakes AIAA-96-4532,1996
3. P.A.Waltrup LiquidFueledSupersonicCombustionRamjets: A Research Perspectiveof the Past, Present, and Future;AIAA-86-0158
4. N.C.Bissinger,D.M.Schmitz Design andWindTunnelTesting ofIntakes for HypersonicVehicles AIAA93-5042,Munich,1993
5. K.Chung,F.Lu HypersonicTurbulentExpansion-Comerwith Shock Impingement;AIAA-92-5101,1992
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