Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro-Array Actuation-Reference-Cited by-同舟云学术

Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro-Array Actuation

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:3rd AIAA Flow Control Conference
language:
Short-container-title:

Author:

Anderson Bernhard¹,Tinapple Jon²,Surber Lewis³

Affiliation:

1. NASA Glenn Research Center

2. Wright-Patterson Air Force Base

3. Universal Technology Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3197

Reference6 articles.

1. (5)NPARCAlliance,"TheWind-USCode",http://www/grc.nasa/www/Wind-US_docs[cited13 June 2004.

2. (6)Bush,R.H.,Power,G.D.,andTowne,C.E."Wind-US:TheProductionFlowSolverofthe NPRACAlliance",AIAA-1998-0935,Januar7y1998.

3. (7)Anderson,B.H.,Tinapple,J.,andSurber,L."OptimalMicro-ArrayActuationControlfor ShockWave BoundaryLayer InteractionsinSupersonic Inlets",ProposedNASATM,2006. Figure(1): Schematic diagramshowingtheshock generator andstandardmicro-rampactuators installedinthe NASA/GRC15x15cm.Supersonic WindTunnel.

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