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.
- Physical Description: 1 online resource (82 pages) : chiefly illustrations.
- Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
Title from title screen (viewed on Aug. 16, 2016).
"Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technolocy Laboratories"--Report documentation page.
|Bibliography, etc. Note:||
Includes bibliographical references (page 13).
|Type of Report and Period Covered Note:||
|Funding Information Note:||
National Aeronautics and Space Administration and U.S. Army Aviation Research and Development Command 505-31-33-02