DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Documentation of Experimental Data for Hypersonic 3-D Shock Waves

Schülein, E. and Zheltovodov, A.A. (2001) Documentation of Experimental Data for Hypersonic 3-D Shock Waves. DLR-Interner Bericht. 99 A 26, 95 S.

Full text not available from this repository.


Experimental data for a series of three-dimensional hypersonic swept- and crossing-shock-waves / turbulent boundary layer interaction flows in the vicinity of one and two sharp fins mounted on a flat plate are presented. The data contains detailed documentation of incoming boundary layer, surface pressure and heat flux distributions, skin friction distributions and topological features of the limiting streamlines in the interaction region at M = 5. The deflection angles ß were varied for swept-shock interactions (single fin geometry) from 0° to 27°, and for crossing-shock interaction (double fin geometry) from 8° to 23°.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2001,
Title:Documentation of Experimental Data for Hypersonic 3-D Shock Waves
AuthorsInstitution or Email of Authors
Zheltovodov, A.A.UNSPECIFIED
Number of Pages:95
Keywords:hypersonic flow, swept shock, crossing shock, turbulent boundary layer,
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Military Technologies
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: elib DLR-Beauftragter
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 18:49

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.