Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions / William J. Devenport, Stewart A.L. Glegg.

Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions / William J. Devenport, Stewart A.L. Glegg.

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Bibliographic Details
Author / Creator:Devenport, William J.
Imprint:[Washington, D.C.] : [National Aeronautics and Space Administration] ; [Springfield, Va. :] : [National Technical Information Service, distributor], [1994]
Description:1 volume.
Language:English
Series:[NASA contractor report] ; NASA CR-195824
NASA contractor report ; NASA CR-195824.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6507404
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Other authors / contributors:United States. National Aeronautics and Space Administration.
Notes:Distributed to depository libraries in microfiche.
Available via Internet from the NTRS web site. Address as of 12/2/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940029701%5F1994029701.pdf; current access is available via PURL.
GPO item no.:0830-H-14 (MF)
0830-H-14 (online)
Govt.docs classification:NAS 1.26:195824

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