Mesoflap and Bleed Flow Control for a Mach 2 Inlet-Reference-Cited by-同舟云学术

Mesoflap and Bleed Flow Control for a Mach 2 Inlet

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Loth Eric¹,Roos Frederick²,Davis Dave³,Mace James²,Jaiman Rajeev¹,White S.¹,Dutton C.¹,Dutton C.¹

Affiliation:

1. University of Illinois at Urbana-Champaign

2. Boeing Phatom Works

3. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-855

Reference15 articles.

1. ACKNOWLEDGMENTS Thisworkwassupportedunder ContractNo. F49620-98-1-0490bytheDefenseAdvancedResearchProjectsAgency (DARPA)withDr.RichardWlezien astechnicalmonitor andthe AirForceOfficeof ScientificResearch(AFOSR) withDr. StevenWalkerastechnical monitor.We would alsoliketo acknowledge(alphabetically):A.Alleyne, P. Guebelle,S.Kim, S.Mcllwain,J. Pittman,andD. Tortorelli. 'Nicolai,L.M.(1975)FundamentalsofAircraftDesign METSInc. SanJose,CA.

2. Anderson,J.(1990)''Airframe/Propulsion Integrationof SupersonicVehicles" 26'hAIAA/SAE/ASME/ASEE Joint Propulsion Conference, AIAA 90-2151,Orlando,FL,July.6E.Loth"SmartMesoflapsforControlofShockBoundary-LayerInteractions,"AZAAFluidDynamics 2000,AIAA200-2476,Denver,CO,June.

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