|
Volumn 39, Issue 4, 2001, Pages 745-748
|
Effects of rotating tabs on flow and acoustic fields of supersonic jet
a a |
Author keywords
[No Author keywords available]
|
Indexed keywords
BOUNDARY LAYERS;
JETS;
NOZZLES;
SUPERSONIC FLOW;
VORTEX FLOW;
ROTATING TABS;
SUPERSONIC JETS;
VORTEX GENERATORS;
SUPERSONIC AERODYNAMICS;
|
EID: 0035311720
PISSN: 00011452
EISSN: None
Source Type: Journal
DOI: 10.2514/2.1373 Document Type: Article |
Times cited : (9)
|
References (6)
|