Flow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96 / by Robert L. Weirich and Walter A. Vahl.

Bibliographic Details
Main Authors: Weirich, Robert L., (Author), Vahl, Walter A., (Author)
Format: Book Government Document
Published: Washington, D.C. : National Aeronautics and Space Administration, October 1968.
Series:NASA technical note ; D-4809.
Online Access:CONNECT