메뉴 건너뛰기




Volumn , Issue , 2008, Pages

Unsteady normal shock wave boundary layer interactions with control

Author keywords

[No Author keywords available]

Indexed keywords

DUCTS; SHOCK WAVES;

EID: 78149431418     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (12)
  • 1
    • 0035245485 scopus 로고    scopus 로고
    • Self-sustained shock oscillations on airfoils at transonic speeds
    • Lee, B.H.K., Self-sustained shock oscillations on airfoils at transonic speeds, Progress in Aerospace Sciences 37, pp147-196, 2001.
    • (2001) Progress in Aerospace Sciences , vol.37 , pp. 147-196
    • Lee, B.H.K.1
  • 2
    • 0021411432 scopus 로고
    • Forced oscillation experiments in supercritical diffuser flows
    • Sajben, M. and Bogar, TJ and Kroutil, JC, Forced oscillation experiments in supercritical diffuser flows, AIAA Journal 22, No. 4, pp465-474, 1984.
    • (1984) AIAA Journal , vol.22 , Issue.4 , pp. 465-474
    • Sajben, M.1    Bogar, T.J.2    Kroutil, J.C.3
  • 3
    • 0029139662 scopus 로고
    • Experimental and numerical study of the time-dependent pressure response of a shock wave oscillating in a nozzle
    • Ott, P. and Bolcs, A. and Fransson, T.H., Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle, Journal of Turbomachinery 117, pp106-114, 1995.
    • (1995) Journal of Turbomachinery , vol.117 , pp. 106-114
    • Ott, P.1    Bolcs, A.2    Fransson, T.H.3
  • 4
    • 0037273437 scopus 로고    scopus 로고
    • Mechanism of shock wave oscillation in transonic diffusers
    • Handa, T. and Masuada, M. and Matsuo, K., Mechanism of Shock Wave Oscillation in Transonic Diffusers, AIAA Journal 41, No. 1 pp64-70, 2003.
    • (2003) AIAA Journal , vol.41 , Issue.1 , pp. 64-70
    • Handa, T.1    Masuada, M.2    Matsuo, K.3
  • 5
    • 33744804319 scopus 로고    scopus 로고
    • Experimental and numerical study of forced shock-wave oscillations in a transonic channel
    • Bur, R. and Benay, R. and Galli, A. and Berthouze, P., Experimental and numerical study of forced shock-wave oscillations in a transonic channel, Aerospace Science and Technology 10, pp265-278, 2006.
    • (2006) Aerospace Science and Technology , vol.10 , pp. 265-278
    • Bur, R.1    Benay, R.2    Galli, A.3    Berthouze, P.4
  • 6
    • 0346770798 scopus 로고
    • An experimental study of the interaction of an unsteady shock with a turbulent boundary layer
    • Edwards, J.A. and Squire, L.C., An experimental study of the interaction of an unsteady shock with a turbulent boundary layer, Aeronautical Journal 97, No. 970, pp337-348, 1993.
    • (1993) Aeronautical Journal , vol.97 , Issue.970 , pp. 337-348
    • Edwards, J.A.1    Squire, L.C.2
  • 8
    • 33751229268 scopus 로고    scopus 로고
    • Wind tunnel setup for investigations of normal shock wave/boundary-layer interaction control
    • Ogawa, H. and Babinsky, H., Wind Tunnel Setup for Investigations of Normal Shock Wave/Boundary-Layer Interaction Control, AIAA Journal 44, No. 11 pp2803-2805, 2006.
    • (2006) AIAA Journal , vol.44 , Issue.11 , pp. 2803-2805
    • Ogawa, H.1    Babinsky, H.2
  • 9
    • 4344605238 scopus 로고    scopus 로고
    • Dynamics and control of shock motion in a near-isentropic inlet
    • MacMartin, D.G., Dynamics and Control of Shock Motion in a Near-Isentropic Inlet, Journal of Aircraft 41, No. 4 pp846-853, 2004.
    • (2004) Journal of Aircraft , vol.41 , Issue.4 , pp. 846-853
    • Mac Martin, D.G.1
  • 10
    • 0026627107 scopus 로고
    • A study of the interaction of a normal shock wave with a turbulent boundary layer at Mach numbers between 1.30 and 1.55
    • Atkin, C.J. and Squire, L.C., A study of the interaction of a normal shock wave with a turbulent boundary layer at Mach numbers between 1.30 and 1.55, European Journal of Mechanics, B/Fluids 11, No. 1, pp93-118, 1992.
    • (1992) European Journal of Mechanics, B/Fluids , vol.11 , Issue.1 , pp. 93-118
    • Atkin, C.J.1    Squire, L.C.2
  • 11
    • 33847724345 scopus 로고    scopus 로고
    • The effect of sub-boundary layer vortex generators on shock/boundary layer interactions
    • Holden, H.A. and Babinsky, H., The effect of sub-boundary layer vortex generators on shock/boundary layer interactions, Journal of Aircraft 44, No. 1 pp170-174, 2007.
    • (2007) Journal of Aircraft , vol.44 , Issue.1 , pp. 170-174
    • Holden, H.A.1    Babinsky, H.2
  • 12
    • 0036588638 scopus 로고    scopus 로고
    • Review of research on low-profile vortex generators to control boundary-layer separation
    • Lin, J., Review of research on low-profile vortex generators to control boundary-layer separation, Progress in Aerospace Sciences, 38 pp389-420, 2002.
    • (2002) Progress in Aerospace Sciences , vol.38 , pp. 389-420
    • Lin, J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.