Periodic Exhaust Flow through a Converging-Diverging Nozzle Downstream of a Rotating Detonation Engine (AIAA 2014-1015)
52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD
2014-01-01
12 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
AIAA-2005-1177 STUDY ON DETONATION STRUCTURE PROPAGATING IN A CONVERGING-DIVERGING NOZZLE
British Library Conference Proceedings | 2005
|