Computational Investigation of Fuel Injection with Various Injector Geometries and Mixing into Hypersonic Crossflow in Scramjet Engines
51st, Aerospace sciences meeting ; 2013 ; Grapevine, TX
2013-01-01
21 pages
Includes bibliographical references and index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
TRANSVERSE INJECTION INTO SUBSONIC CROSSFLOW WITH VARIOUS INJECTOR ORIFICE GEOMETRIES
British Library Conference Proceedings | 2010
|British Library Conference Proceedings | 2004
|