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Effect of wall suction on the stability of compressible subsonic flows over smooth two-dimensional backward-facing stepsThe effect of suction on the stability of compressible flows over backward-facing steps is investigated. Mach numbers up to 0.8 are considered. The results show that continuous suction stabilizes the flow outside the separation bubble, but it destabilizes the flow inside it. Nevertheless, the overall N factor decreases as the suction level increases due to the considerable reduction of the separation bubble. For the same suction flow rate, properly distributed suction strips stabilize the flow more than continuous suction. The size of the separation bubble, and hence its effect on the instability can be considerably reduced by placing strips with high suction velocities in the separation region.
Document ID
19890043124
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Al-Maaitah, Ayman A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Nayfeh, Ali H.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Ragab, Saad A.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 14, 2013
Publication Date
March 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 89-0983
Accession Number
89A30495
Funding Number(s)
CONTRACT_GRANT: N00014-85-K-0011
CONTRACT_GRANT: NAG1-714
Distribution Limits
Public
Copyright
Other

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