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Volumn 14, Issue 3, 2006, Pages 211-231

An inverse blade design method for subsonic and transonic viscous flow in compressors and turbines

Author keywords

Aerodynamic shape design; ALE formulation; Inverse blade design; Moving mesh; Reynolds averaged Navier Stokes

Indexed keywords


EID: 33244485476     PISSN: 10682767     EISSN: None     Source Type: Journal    
DOI: 10.1080/17415970500354235     Document Type: Article
Times cited : (30)

References (19)
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.