Computational Investigation of the Upsweep Flow Field for a Simplified C-130 Shape-Reference-Cited by-同舟云学术

Computational Investigation of the Upsweep Flow Field for a Simplified C-130 Shape

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Bergeron Keith¹,Cassez Jean-Francois¹,Bury Yannick²

Affiliation:

1. U.S. Air Force Academy

2. Institut Superieur de l'Aeronautique et de l'Espace

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-90

Reference12 articles.

1. 1Seeger,M.,Muller,L.,Carlsson,P.K.,Bury,Y.,Pressigny,Y.,Lallemand,G.,Vallance, M., Wheeler,R.,andBenney,R."Four-Power LongTermTechnologyProjects:Airflow InfluenceonAirdropand2ndPrecisionAirdropImprovements",AIAA2005-1602

2. 2Wooten,J.D.andYechout,T.R."WindTunnelEvaluationofC-130DragReduction StrakesandIn-flight LoadLoadingPrediction",AIAA 2008-348

3. 3Claus,M.P.,Morton,S.A.,Cummings,R.M.,andBury,Y."DESTurbulenceModeling on the C-130ComparisonbetweenComputational andExperimental Results",AIAA2005-884

4. 5Bury,Y.,Morton,S.A.,Charles,R."ExperimentalInvestigationoftheFlowfieldinthe CloseWakeofaSimplifiedC-130Shape,AModel Approachof AirflowInfluenceonAirdrop", AIAA2008-6415

5. A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities

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