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Volumn 21, Issue 9, 1983, Pages 1232-1240

Characteristic frequencies of transonic diffuser flow oscillations

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS - TRANSONIC; SHOCK WAVES - ANALYSIS;

EID: 0020824612     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.8234     Document Type: Article
Times cited : (146)

References (20)
  • 2
    • 0017790316 scopus 로고
    • Unsteady Transonic Flow in a Two-Dimensional Diffuser
    • AGARD Conference Proceedings No. 227
    • Sajben, M., Kroutil, J. C., and Chen, C. P., “Unsteady Transonic Flow in a Two-Dimensional Diffuser,” Unsteady Aerodynamics, AGARD Conference Proceedings No. 227, 1977, pp. 13-1 to 13-14.
    • (1977) Unsteady Aerodynamics
    • Sajben, M.1    Kroutil, J.C.2    Chen, C.P.3
  • 3
    • 0018529316 scopus 로고
    • Shock-Wave Oscillations in a Transonic Diffuser Flow
    • Chen, C. P., Sajben, M., and Kroutil, J. C., “Shock-Wave Oscillations in a Transonic Diffuser Flow,” AIAA Journal, Vol. 17, Oct. 1979, pp. 1076-1083.
    • (1979) AIAA Journal , vol.17 , pp. 1076-1083
    • Chen, C.P.1    Sajben, M.2    Kroutil, J.C.3
  • 4
    • 0019634239 scopus 로고
    • Effects of Initial Boundary-Layer Thickness on Transonic Diffuser Flows
    • Sajben, M. and Kroutil, J. C., “Effects of Initial Boundary-Layer Thickness on Transonic Diffuser Flows,” AIAA Journal, Vol. 19, Nov. 1981, pp. 1386-1393.
    • (1981) AIAA Journal , vol.19 , pp. 1386-1393
    • Sajben, M.1    Kroutil, J.C.2
  • 7
    • 0019382598 scopus 로고
    • Improved Calculations of High Speed Inlet Flows, Part I: Numerical Algorithm
    • Knight, D. D., “Improved Calculations of High Speed Inlet Flows, Part I: Numerical Algorithm,” AIAA Journal, Vol. 19, Jan. 1981, pp. 34-41.
    • (1981) AIAA Journal , vol.19 , pp. 34-41
    • Knight, D.D.1
  • 8
    • 85003220392 scopus 로고
    • Improved Calculation of High Speed Inlet Flows, Part II: Results
    • Knight, D. D., “Improved Calculation of High Speed Inlet Flows, Part II: Results,” AIAA Journal, Vol. 19, Feb. 1981, pp. 172-179.
    • (1981) AIAA Journal , vol.19 , pp. 172-179
    • Knight, D.D.1
  • 10
    • 0000250414 scopus 로고
    • Shock-Induced Separation and Its Prevention by Design and Boundary Layer Control
    • edited by G. V. Lachmann, Pergamon Press, New York
    • Pearcey, H. H., “Shock-Induced Separation and Its Prevention by Design and Boundary Layer Control,” Boundary Layer and Flow Control, Vol. 2, edited by G. V. Lachmann, Pergamon Press, New York, 1961.
    • (1961) Boundary Layer and Flow Control , vol.2
    • Pearcey, H.H.1
  • 11
    • 0019354024 scopus 로고
    • Flow in Transonic Compressors
    • Kerrebrock, J. L., “Flow in Transonic Compressors,” AIAA Journal, Vol. 19, Jan. 1981, pp. 4-19.
    • (1981) AIAA Journal , vol.19 , pp. 4-19
    • Kerrebrock, J.L.1
  • 16
    • 85003361443 scopus 로고
    • Real-Time Optical Measurement of Time-Dependent Shock Position
    • Sajben, M. and Crites, R. C., “Real-Time Optical Measurement of Time-Dependent Shock Position,” AIAA Journal, Vol. 17, Aug. 1979, pp. 910-912.
    • (1979) AIAA Journal , vol.17 , pp. 910-912
    • Sajben, M.1    Crites, R.C.2
  • 18
    • 77956831639 scopus 로고
    • Analytical Procedure for the Calculation of Attached and Separated Subsonic Diffuser Flows
    • Bower, W. W., “Analytical Procedure for the Calculation of Attached and Separated Subsonic Diffuser Flows,” Journal of Aircraft, Vol. 13, Jan. 1976, pp. 49-56.
    • (1976) Journal of Aircraft , vol.13 , pp. 49-56
    • Bower, W.W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.