Helicopter model rotor-blade vortex interaction impulsive noise : scalability and parametric variations / W.R. Splettstoesser ... [et al.].

Format Microform
Publication InfoMoffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Systems Command, [1984]
Descriptionii, 28 p. : ill.
Supplemental Contenthttps://purl.fdlp.gov/GPO/LPS101194
Subjects

Other author/creatorSplettstoesser, W. R.
Other author/creatorDeutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt.
Other author/creatorArmy Research and Technology Laboratories (U.S.)
Other author/creatorAmes Research Center.
SeriesNASA technical memorandum ; 86007
NASA technical memorandum 86007. ^A467613
Abstract Acoustic data taken in the anechoic Deutsch-Niederlaendischer Windkanal (DNW) have documented the blade-vortex interaction (BVI) impulsive noise radiated from a 1/7-scale model main rotor of the AH-1 series helicopter.
General note"Report date December 1984."
General noteGPO Cataloging Record Distribution Program (CRDP).
Other formsAlso available via Internet from the NTRS web site. Address as of 09/02/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850008517%5F1985008517.pdf ; current access is available via PURL.
Reproduction noteMicrofiche. [Washington, D.C. : National Aeronautics and Space Administration], 1985. 1 microfiche.
GPO item number0830-D (MF)
GPO item number0830-D (online)
Govt. docs number NAS 1.15:86007
Stock numberN 85-16826 NASA

Availability

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Joyner Microforms B300 NAS 1.15:86007 ✔ Available