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Volumn , Issue , 1997, Pages

The application of cfd to the prediction of missile body vortices

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; ANGLE OF ATTACK; CYLINDER CONFIGURATIONS; FLOW FIELDS; FORECASTING; LAMINAR FLOW; MISSILES; STRAIN GAGES; TURBULENCE MODELS; WATER CRAFT;

EID: 84982318599     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (30)

References (8)
  • 4
    • 44949269885 scopus 로고
    • Computing Aerodynamics Methodology for the Aerospace Plane
    • Chakravarthy, S. R., et. al., "Computing Aerodynamics Methodology for the Aerospace Plane," Computing Systems in Engineering, Vol. 1, Nos 2-4, pp. 415-435, 1990.
    • (1990) Computing Systems in Engineering , vol.1 , Issue.2-4 , pp. 415-435
    • Chakravarthy, S.R.1
  • 5
    • 0028486597 scopus 로고
    • Onset of Vortex Breakdown Above a Pitching Delta Wing
    • August
    • Visbal, M.R., "Onset of Vortex Breakdown Above a Pitching Delta Wing," AIAA Journal, 32(8), pp. 1568-1575, August 1995.
    • (1995) AIAA Journal , vol.32 , Issue.8 , pp. 1568-1575
    • Visbal, M.R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.