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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.

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Record details

  • 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.

Content descriptions

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, etc. Note: Includes bibliographical references (page 13).
Type of Report and Period Covered Note: Technical paper.
Funding Information Note: National Aeronautics and Space Administration and U.S. Army Aviation Research and Development Command 505-31-33-02
L-13139

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