Experimental Investigations of Reconfigurable Porosity for Aerodynamic Control-Reference-Cited by-同舟云学术

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Experimental Investigations of Reconfigurable Porosity for Aerodynamic Control

Published:2004-06-20 Issue: Volume: Page:
ISSN:
Container-title:2nd AIAA Flow Control Conference
language:
Short-container-title:

Author:

Lopera Javier¹,Terry Tsun-Ming¹,Patel Mehul²

Affiliation:

1. University of Toledo

2. Orbital Research Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2695

Reference11 articles.

1. 1Bahi,L.,andRoss,J.M."PassiveShockWave/BoundaryLayerControlForTransonicAirfoilDragReduction," AIAAPaper1983-0137,January1983.

2. 2Raghunathan,S."PassiveShockwaveBoundaryLayerControlExperimentsonaCircularArcModel,"AIAA Paper1986-0285,January1986.

3. 3Nagamatsu,H.T.,Trilling,T.W.,andBossard,J.A."PassiveDragReductiononaCompleteNACA0012Airfoil atTransonicMachNumbers,"AIAA Paper1987-1263,June1987.

4. 4Chen,C.L.,Chow,C.Y.,VanDalsem,W.,andHolst,T."ComputationofViscous TransonicFlowoverPorous Airfoils,"AIAA Paper1987-0359,January1987.

5. 5Wood,R.M.,Banks,D.W.,andBauer,S.X.S."AssessmentofPassivePorositywithFree andFixedSeparation onaTangentOgiveForebody,"AIAA Paper1992-4494,1992.

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