Prediction of flow separation on launch vehicle configurations
Author:
Affiliation:
1. McDonnell Douglas Research Laboratories, Saint Louis MO
2. McDonnell Douglas Space Systems Co., Delta Launch Vehicle Div., Huntington Beach, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1727
Reference15 articles.
1. Wang,J.C.T,Than,P.T.andWidhopf,G.F."Multi-BodyLaunchVehicleFlowfieldSimulation,"AIAA Paper 91-0072, Jan. 1991.
2. Viscous transonic airfoil workshop compendium of results
3. Deese,J.E.andAgarwal,R. K."Navier-Stokes Calculations ofTransonicFlowAboutWinglSody Configurations,"loumal ofAircraft,Vol.25, 1988,pp. 1106-1112.
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