Shock fitting applied to the prediction of high-speed rotor noise
By: Major John W. Rutherford.
Contributors: Ames Research Center.; United States. Army Aviation Systems Command.
Series: NASA technical memorandum -- 86781.; USAAVSCOM technical report -- TR 85-A-8.; AVSCOM technical report -- 85-A-8.
Publisher: National Aeronautics and Space Administration, Ames Research Center; United States Army Aviation Systems Command; For sale by the National Technical Information Service
Published: 1985
Place of publication: Moffett Field, Calif; St. Louis, Mo; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics, Transonic.; Rotors (Helicopters)
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1985. 1 microfiche.