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Control and reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interactionThe focus was on developing means of controlling and reducing unsteady pressure loads in separated shock wave turbulent boundary layer interactions. Section 1 describes how vortex generators can be used to effectively reduce loads in compression ramp interaction, while Section 2 focuses on the effects of 'boundary-layer separators' on the same interaction.
Document ID
19960009427
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Authors
Dolling, David S. (Texas Univ. Austin, TX, United States)
Barter, John W. (Texas Univ. Austin, TX, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-199334
NAS 1.26:199334
Report Number: NASA-CR-199334
Report Number: NAS 1.26:199334
Accession Number
96N16593
Funding Number(s)
CONTRACT_GRANT: NAG1-1471
Distribution Limits
Public
Copyright
Public Use Permitted.

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