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