NUMERICAL DESIGN STUDY OF SCRAMJET ISOLATOR CROSS-SECTIONAL SHAPE TRANSITION WITH VARIED DIVERGENCE ANGLE
16th, International symposium on air breathing engines ; 2003 ; Cleveland, Ohio
01.01.2003
1252 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2017
|A COMPARISON STUDY OF RECTANGULAR AND CHAMFERED ISOLATOR CROSSECTIONAL SHAPE WITH VARIED DIVERGENCE
British Library Conference Proceedings | 2004
|NUMERICAL ANALYSIS OF SCRAMJET INTAKE WITH SPOON-SHAPED ISOLATOR
TIBKAT | 2021
|