Numerical Study of Pressure Fluctuations due to a Mach 6 Turbulent Boundary Layer
51st, Aerospace sciences meeting ; 2013 ; Grapevine, TX
2013-01-01
16 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
A High Mach Number Turbulent Boundary-Layer Study
AIAA | 1976
|Numerical Simulation of Wall-Pressure Fluctuations Due to a Turbulent Boundary Layer
Online Contents | 2012
|