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Volumn , Issue , 2003, Pages

Implementation and benefits of variable geometry wings for a supersonic business jet

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894428513     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (7)

References (17)
  • 1
    • 84894480487 scopus 로고    scopus 로고
    • Defense Advanced Research Project Agency, DARPA VA
    • Defense Advanced Research Project Agency Quiet Supersonic Platform, DARPA VA
    • Quiet Supersonic Platform
  • 6
    • 84894489866 scopus 로고    scopus 로고
    • Engineous Software
    • Engineous Software, iSight Engineous Software, NC http://www.engineous.com/index.htm
    • ISight Engineous Software
  • 7
    • 84894496116 scopus 로고    scopus 로고
    • Phoenix Integration, Phoenix Integration, VA
    • Phoenix Integration, Model Center Basic, Phoenix Integration, VA 2002
    • (2002) Model Center Basic
  • 10
    • 84873824845 scopus 로고    scopus 로고
    • Red Hat, Inc
    • Red Hat, Inc. Cygwin User's Guide Red Hat, Inc. http://www.cygwin.com/cygwin-ug-net/cygwin-ugnet.html
    • Cygwin User's Guide
  • 13
    • 27744601994 scopus 로고    scopus 로고
    • Aeropropulsion Office, NASA Lewis Research Center, Cleveland Ohio, March
    • Klann J. L., Snyder C. A., NASA Engine Performance Program, Aeropropulsion Office, NASA Lewis Research Center, Cleveland Ohio, March 1997
    • (1997) NASA Engine Performance Program
    • Klann, J.L.1    Snyder, C.A.2
  • 14
    • 33748693557 scopus 로고
    • Boeing Military Airplane Development, NASA Glenn Research Center, PSAO office
    • Boeing Military Airplane Development, NASA Glenn Research Center, PSAO office Weight Analysis of Turbine Engine 1979
    • (1979) Weight Analysis of Turbine Engine


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.