Helicopter rotor blade computation in unsteady flows using moving overset grids
By: Jasim Ahmad and Earl P.N. Duque.
Contributors: Duque, Earl P. N.; United States. National Aeronautics and Space Administration.
Series: [NASA technical memorandum] -- 207307.
Publisher: American Institute of Aeronautics and Astronautics; [National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Blade-vortex interaction.; Rotary wing aircraft.; Computational fluid dynamics.; Computational grids.; Unsteady flow.; Helicopters.; Dynamic models.
Notes: Shipping list no.: 99-0618-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.