Helicopter blade dynamic loads measured during performance testing of two scaled rotors
By: John D. Berry.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical memorandum -- 89053; AVSCOM technical memorandum -- 87-B-7
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; National Technical Information Service, distributor]
Published: 1987
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 45
Subjects: Dynamic loads.; Helicopters.; Rotors.; Rotors (Helicopters) -- Testing.; Rotors (Helicopters) -- Aerodynamics.; Scaling.; Wind tunnel models.
Notes: Cover title.

Distributed to depository libraries in microfiche.

Includes bibliographical references (p. 7).

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1987] 1 microfiche : negative.