Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /

Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /

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Bibliographic Details
Author / Creator:	Noonan, Kevin W., author.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
Description:	1 online resource (82 pages) : chiefly illustrations.
Language:	English
Series:	NASA technical paper ; 1701 AVRADCOM technical report ; 80-B-5 NASA technical paper ; 1701. AVRADCOM technical report ; 80-B-5.
Subject:	Aerofoils -- Testing. Helicopters -- Aerodynamics. Reynolds number. Rotors (Helicopters) -- Testing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10914300

Hidden Bibliographic Details
Other authors / contributors:	Bingham, Gene J., author. Langley Research Center. United States. Army Aviation Research and Development Command. Army Research and Technology Laboratories (U.S.). Structures Laboratory. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Notes:	Title from title screen (viewed on Aug. 16, 2016). "September 1980." "Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technolocy Laboratories"--Report documentation page. Includes bibliographical references (page 13). Technical paper. National Aeronautics and Space Administration and U.S. Army Aviation Research and Development Command 505-31-33-02 L-13139
Other form:	Print version: Noonan, Kevin W. Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 Microfiche version: Noonan, Kevin W. Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:1701

Description
Item Description:	Title from title screen (viewed on Aug. 16, 2016). "September 1980." "Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technolocy Laboratories"--Report documentation page.
Physical Description:	1 online resource (82 pages) : chiefly illustrations.
Bibliography:	Includes bibliographical references (page 13).