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Title	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 /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo71094
Author	Noonan, Kevin W., author.
Published	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.

SuDoc Number	NAS 1.60:1701
Item Number	0830-H-15 (online)
Description	1 online resource (82 pages) : chiefly illustrations.
Content Type	text
Series	(NASA technical paper ; 1701.)
	(AVRADCOM technical report ; 80-B-5.)
General Note	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.
Bibliography	Includes bibliographical references (page 13).
Added Entry	Bingham, Gene J., author.
Added Entry	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.
Linking Field	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 (OCoLC)7363586
	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 (OCoLC)711544725
URL	http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19800023826.pdf

Holdings	All items

OCLC Number	(OCoLC)785231998
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=000991544&local_base=GPO01PUB
System Number	000991544

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