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Stability of compressible three-dimensional boundary-layer flowsFor compressible three-dimensional flow, the method of multiple scales to formulate the three-dimensional stability problem and determine the partial-differential equations governing variations of the amplitude and complex wavenumbers is used. A method for following one specific wave along its trajectory to ascertain the characteristics of the most unstable disturbance is proposed. Numerical results using the flow over the X-21 wing as calculated from the Kaups-Cebeci code will be presented.
Document ID
19820053941
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reed, H. L. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Nayfeh, A. H. (Virginia Polytechnic Institute and State University Blacksburg, VA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 82-1009
Meeting Information
Meeting: Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference
Location: St. Louis, MO
Start Date: June 7, 1982
End Date: June 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics and American Society of Mechanical Engineers
Accession Number
82A37476
Funding Number(s)
CONTRACT_GRANT: NSG-1255
CONTRACT_GRANT: N00014-75-C-0381
Distribution Limits
Public
Copyright
Other

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