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Volumn , Issue , 1999, Pages

Wave drag extraction from profile drag based on a wake-integral method

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; DRAG; ENTROPY; EXTRACTION; FLOW FIELDS; SHOCK WAVES; SUPERSONIC AIRCRAFT; SURVEYS; VORTICITY;

EID: 84983178051     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-275     Document Type: Conference Paper
Times cited : (18)

References (13)
  • 1
    • 0002546443 scopus 로고
    • A Method for the Direct Determination of Profile Drag (In German)
    • Betz, A."A Method for the Direct Determination of Profile Drag (in German)" ZFM, Vol. 16, pp. 42, 1925.
    • (1925) ZFM , vol.16 , pp. 42
    • Betz, A.1
  • 3
    • 0028397339 scopus 로고
    • Quantitative Low-Speed Wake Surveys
    • March-April
    • Brune, G. W."Quantitative Low-Speed Wake Surveys" Journal of Aircraft Vol. 31, No. 2, March-April 1994.
    • (1994) Journal of Aircraft , vol.31 , Issue.2
    • Brune, G.W.1
  • 12
    • 0003649544 scopus 로고
    • Academic Press, Inc., New York
    • Oswatitsch, K., GAS DYNAMICS, Academic Press, Inc., New York, 1956.
    • (1956) GAS DYNAMICS
    • Oswatitsch, K.1
  • 13
    • 0024630852 scopus 로고
    • University of Tronto Institute for Aerospace Studies (UTIAS) Technical Note No. 270
    • Smith, D. S., "Flow Characteristics About a Trailing Edge" University of Tronto Institute for Aerospace Studies (UTIAS) Technical Note No. 270, 1989.
    • (1989) Flow Characteristics about a Trailing Edges
    • Smith, D.S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.