Surface Flow and PSP Measurements in the Large-Scale Low-Boom Inlet (Invited)
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3799
Reference36 articles.
1. 1Conners,T.R.,andHowe,D.C."SupersonicInletShapingforDramaticReductioninDragandSonicBoomStrength,"44thAIAAAerospaceSciencesMeetingand Exhibit, AIAAPaper 2006-30,2006.
2. 3Tacina,K.M.,Hirt,S.M.,Conners,T.R.,Merret,J.M.,andHowe,D.C."DynamicAnalysisofWindTunnelDatafrom IsentropicRelaxed Compression Inlet,"43rdAIAA/ASME/SAE/ASEEJointPropulsionConference,AIAAPaper2007-5073, 2007.
3. 4Hirt, S.M., Tacina, K.M., Conners, T.R., Merret, J.M., and Howe, D.C. "CFD Results for an Axisymmetric Isentropic Relaxed Compression Inlet,"46thAIAAAerospaceSciencesMeetingandExhibit,AIAAPaper2008-92,2008.
4. Interactions between shock waves and turbulent boundary layers
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1. Aerodynamic Impact of Vortex Generators on a Relaxed-Compression Low-Boom Inlet;AIAA Journal;2015-12
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