Turbulent boundary-layer wall pressure fluctuations downstream of a tandem LEBU
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9331
Reference8 articles.
1. Interior noise radiated by an airplane fuselage subjected to turbulent boundary layer excitation and evaluation of noise reduction treatments
2. Performance of large-eddy breakup devices at post-transitional Reynolds numbers
3. 5Thomas, A.S.W. "Organized Structures in the Turbulent Boundary Layer," Ph.D. Dissertation,University of South Adelaide, Australia, 1977.
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2. Effects of a Large Eddy Breakup Device on the Fluctuating Wall Pressure Field (Data Bank Contribution);Journal of Fluids Engineering;1993-09-01
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