A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory /

A comparison is made of the theoretical and experimental subsonic compressible pressure-coefficient distributions about several bodies in revolution. The results show that the linearized theory predicts the subsonic pressure coefficients over the central portion of the body. An extrapolation of the...

Full description

Bibliographic Details
Main Author: Matthews, Clarence W
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : U.S. G.P.O., 1953
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2519
Subjects:

Internet

This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.

Stanford University

Holdings details from Stanford University
Call Number: NACA TN 2519