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 / Kevin W. Noonan and Gene J. Bingham.
Publication Info.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
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).
Access
Use copy Restrictions unspecified star MiAaHDL
Type Of Report
Technical paper.
Reproduction
Electronic reproduction. [S.l.] : HathiTrust Digital Library, 2011. MiAaHDL
Funding
National Aeronautics and Space Administration and U.S. Army Aviation Research and Development Command 505-31-33-02
L-13139
System Details
Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212 MiAaHDL
Processing Action
digitized 2011 HathiTrust Digital Library committed to preserve pda MiAaHDL
