Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
By: J.D. Baeder.
Contributors: Ames Research Center.; United States. Army Aviation Research and Technology Activity.
Series: NASA technical memorandum -- 103837; USAAVSCOM technical memorandum -- 90-A-007; AVSCOM technical memorandum -- 90-A-7.
Publisher: National Aeronautics and Space Administration, Ames Research Center; US Army Aviation Systems Command, Aviation Research and Technology Activity; For sale by the National Technical Information Service, distributor
Published: 1991
Place of publication: Moffett Field, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Acoustic properties.; Blade tips.; Computational fluid dynamics.; Euler equations of motion.; Hovering.; Nonlinearity.; Rotor aerodynamics.; Rotor blades (Turbomachinery); Stability.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.