Research Catalog

Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions

Title
Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions [microform] / principle investigators: William J. Devenport, Stewart A.L. Glegg.
Author
Devenport, William J.
Publication
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]

Details

Additional Authors
United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA contractor report ; NASA CR-195824
Subject
  • Aeroacoustics
  • Aircraft noise
  • Blade-vortex interaction
  • Noise prediction
  • Vortex shedding
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 94-0864-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:195825
OCLC
marcive32031695
Author
Devenport, William J.
Title
Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions [microform] / principle investigators: William J. Devenport, Stewart A.L. Glegg.
Imprint
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
Series
NASA contractor report ; NASA CR-195824
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.
Added Author
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:195825
Research Call Number
READEX Microfiche NAS 1.26:195825
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