Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade
By: Kevin W. Noonan.
Contributors: United States. Army. Aerostructures Directorate.; Langley Research Center.
Series: NASA technical paper -- 3009.; AVSCOM [technical report] -- TR-90-B-005.; AVSCOM technical report -- 90-B-005.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1990
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 86
Subjects: Rotors (Helicopters) -- Aerodynamics.; Aerofoils -- Testing -- Statistics.; Aerodynamic characteristics.; Aerodynamic coefficients.; Rotary wing aircraft.; Rotary wings.
Genres: Statistics.
Notes: Prepared at the Aerostructures Directorate, USAARTA-AVSCOM, Langley Research Center.

Includes bibliographical references (p. 12-13).

Also available via Internet from the NASA Technical Report Server web site. Address as of 12/07/05:  http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900014923%5F1990014923.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 2 microfiches.