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Volumn , Issue , 2005, Pages

Efficient control of separation using microjets

Author keywords

[No Author keywords available]

Indexed keywords

ADVERSE PRESSURE GRADIENT; AIRCRAFT PROPULSION SYSTEMS; BOUNDARY-LAYER SEPARATION; EFFICIENT CONTROL; ENGINE INLETS; EXPERIMENTAL INVESTIGATIONS; PARAMETRIC SPACES; UNSTEADY PRESSURE MEASUREMENTS;

EID: 78549249483     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (21)

References (21)
  • 4
    • 0030197223 scopus 로고    scopus 로고
    • Delay of Airfoil Stall by Periodic Excitation
    • Wygnanski, Seifert A., "Delay of Airfoil Stall by Periodic Excitation" AIAA J Aircraft 1996; Vol. 33(4):691-8.
    • (1996) AIAA J Aircraft , vol.33 , Issue.4 , pp. 691-698
    • Wygnanski, S.A.1
  • 6
    • 0036651009 scopus 로고    scopus 로고
    • Separation control in duct flows
    • July-August
    • Amitay M., Pitt D., Glezer A. "Separation control in duct flows", Journal of Aircraft Vol. 39, No. 4, July-August 2002.
    • (2002) Journal of Aircraft , vol.39 , Issue.4
    • Amitay, M.1    Pitt, D.2    Glezer, A.3
  • 9
    • 0034291016 scopus 로고    scopus 로고
    • The Control of Flow Separation by Periodic Excitation
    • Greenblatt David, Wygnanski, I.J., "The Control of Flow Separation by Periodic Excitation", Progress in Aerospace Sciences Vol. 36(2000), p. 487-545.
    • (2000) Progress in Aerospace Sciences , vol.36 , pp. 487-545
    • David, G.1    Wygnanski, I.J.2
  • 10
    • 0036588638 scopus 로고    scopus 로고
    • Review of Research on Low Profile Vortex Generators to control Boundary Layer Separation
    • Lin, John C. "Review of Research on Low Profile Vortex Generators to control Boundary Layer Separation", Progress in Aerospace Sciences Vol. 38(2002), p. 389-420.
    • (2002) Progress in Aerospace Sciences , vol.38 , pp. 389-420
    • Lin, J.C.1
  • 11
    • 0029373403 scopus 로고
    • Experimental Study of Lift-Enhancing Tabs on a Two-Element Airfoil
    • Storms B. L, Ross JC. "Experimental Study of Lift-Enhancing Tabs on a Two-Element Airfoil. " AIAA J Aircraft 1995; Vol. 32: 1072-8
    • (1995) AIAA J Aircraft , vol.32 , pp. 1072-1078
    • Storms, B.L.1    Ross, J.C.2
  • 13
    • 0042813602 scopus 로고    scopus 로고
    • Control of Supersonic Impinging Jet Flows using Microjets
    • Alvi, F. S., Elavarsan R., Shih, C., Garg G., and Krothapalli, A., "Control of Supersonic Impinging Jet Flows using Microjets, " AIAA Journal, 2003 Vol. 41(7), p. 1347-1355.
    • (2003) AIAA Journal , vol.41 , Issue.7 , pp. 1347-1355
    • Alvi, F.S.1    Elavarsan, R.2    Shih, C.3    Garg, G.4    Krothapalli, A.5
  • 14
    • 84894617551 scopus 로고    scopus 로고
    • Use of Supersonic Microjets for active separation control in Diffusers
    • Orlando, June 23-26
    • Kumar, V., Alvi, F.S. "Use of Supersonic Microjets for active separation control in Diffusers", AIAA 2003-4160, 33rd AIAA conference, Orlando, June 23-26, 2003.
    • (2003) AIAA 2003-4160, 33rd AIAA conference
    • Kumar, V.1    Alvi, F.S.2
  • 15
    • 84958430400 scopus 로고
    • The Prediction of Separation of Turbulent Boundary Layer
    • Stratford, B.S., "The Prediction of Separation of Turbulent Boundary Layer", J. Fluid Mech. 5, 1-16, 1959b.
    • (1959) J. Fluid Mech. , vol.5 , pp. 1-16
    • Stratford, B.S.1
  • 18
    • 0025449348 scopus 로고
    • Vortex Generator Jets-Means for Flow Separation Control
    • Johnston J.P., Nishi M., "Vortex Generator Jets-Means for Flow Separation Control", AIAA Journal, 1990 Vol. 28, No. 6, pp.989-994.
    • (1990) AIAA Journal , vol.28 , Issue.6 , pp. 989-994
    • Johnston, J.P.1    Nishi, M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.