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Volumn 14, Issue 4, 1971, Pages 439-457

Flight test measurement of exterior turbulent boundary layer pressure fluctuations on Boeing model 737 airplane

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT, NOISE; FLOW OF FLUIDS, TURBULENT;

EID: 0015020279     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/0022-460X(71)90574-8     Document Type: Article
Times cited : (83)

References (19)
  • 5
    • 30244560873 scopus 로고
    • The response of a SST fuselage to boundary layer and to reverberant noise
    • (1969) J. Sound Vib. , vol.9 , pp. 6
    • Crocker1
  • 9
    • 84913092844 scopus 로고
    • Flight measurements of pressure fluctuations in a turbulent subsonic boundary layer and the relation with wall shear stress
    • (1966) R.A.E. tech. Rep. 66338
    • Heron1    Webb2
  • 17
    • 84867800442 scopus 로고
    • Power- and cross-spectra and space-time correlations of surface fluctuating pressures at Mach numbers between 1·6 and 2·5
    • New York, 4th printing, Paper 68–77
    • (1968) AIAA 6th Aerospace Sciences Meeting
    • Chyu1    Hanly2
  • 18
    • 84913086351 scopus 로고
    • An analytical study of the measured wall pressure field under supersonic turbulent boundary layers
    • (1968) NASA CR-888
    • Black1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.