Large-scale advanced propeller blade pressure distributions : predictions and data /

Bibliographic Details
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Nallasamy, M.
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, D.C.] : NASA ; [1989?]
Series:	NASA technical memorandum ; 102316.
Subjects:	Finite difference theory. Finite volume method. Leading edges. Pressure distribution. Propeller blades. Vortices.
Online Access:	https://purl.fdlp.gov/GPO/LPS66323

Description
Item Description:	"AIAA-89-2696" Shipping list number: 90-0893-M. Microform.
Physical Description:	1 volume 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.