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ElectronicResource GovDoc
Author Devenport, William J.

Title Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions [electronic resource] / principle investigators: William J. Devenport, Stewart A.L. Glegg.

Imprint [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:195824    ---  Available
Description 1 v.
Series [NASA contractor report] ; NASA CR-195824
Form Mode of access via Internet from the NTRS web site.
Subject Aeroacoustics.
Aircraft noise.
Blade-vortex interaction.
Noise prediction.
Vortex shedding.
Added Author United States. National Aeronautics and Space Administration.
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:195824

 
    
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