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Volumn 39, Issue 4, 2001, Pages 745-748

Effects of rotating tabs on flow and acoustic fields of supersonic jet

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; JETS; NOZZLES; SUPERSONIC FLOW; VORTEX FLOW;

EID: 0035311720     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1373     Document Type: Article
Times cited : (9)

References (6)


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.