Large-scale advanced propeller blade pressure distributions
Subtitle: predictions and data
By: M. Nallasamy ... [et al.] ; prepared for the 25th Joint Propulsion Conference cosponsored by the AIAA, ASME, SAE, and ASEE, Monterey, California, July 10-12, 1989.
Contributors: Nallasamy, M.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 102316.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1989
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Finite difference theory.; Finite volume method.; Leading edges.; Pressure distribution.; Propeller blades.; Vortices.
Other titles: Large scale advanced propeller blade pressure distributions.
Notes: Shipping list no.: 90-0893-M.

Also available via Internet from the NASA Technical Report Server web site. Address as of 1/13/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013248%5F1990013248.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche.