메뉴 건너뛰기




Volumn 78, Issue 3-4, 2007, Pages 365-382

Generic transport aft-body drag reduction using active flow control

Author keywords

Actuators; Drag reduction; Flow control; Helicopters; Separation bubble; Transport planes; Vortex system; Wake unsteadiness

Indexed keywords

ACTUATORS; AERODYNAMICS; FLOW CONTROL; FLOW SEPARATION; HELICOPTERS; TRANSPORT AIRCRAFT; WAKES;

EID: 34547274815     PISSN: 13866184     EISSN: 15731987     Source Type: Journal    
DOI: 10.1007/s10494-007-9070-x     Document Type: Article
Times cited : (29)

References (8)
  • 1
    • 22544440619 scopus 로고    scopus 로고
    • Delta wing stall and roll control using segmented piezoelectric fluidic actuators
    • May-June; previously AIAA paper 2002-3270
    • Margalit, S., Greenblatt, D., Seifert, A., Wygnanski, I.: Delta wing stall and roll control using segmented piezoelectric fluidic actuators. J. Aircr. 42(3), 698-709 (2004) (May-June; previously AIAA paper 2002-3270)
    • (2004) J. Aircr , vol.42 , Issue.3 , pp. 698-709
    • Margalit, S.1    Greenblatt, D.2    Seifert, A.3    Wygnanski, I.4
  • 2
    • 34547259337 scopus 로고    scopus 로고
    • Naim, A., Seifert, A., Wygnanski, I.: Active control of cylinder flow with and without a splitter plate using piezoelectric actuators. In: AIAA Paper 2002-3070, June 2002 (Submitted in part to J. FTC, 2005)
    • Naim, A., Seifert, A., Wygnanski, I.: Active control of cylinder flow with and without a splitter plate using piezoelectric actuators. In: AIAA Paper 2002-3070, June 2002 (Submitted in part to J. FTC, 2005)
  • 3
    • 85088756422 scopus 로고    scopus 로고
    • Analysis of a boundary layer separation over a bump using large eddy simulation. In: AIAA paper 2001-2558
    • Anaheim, CA
    • Arad, E.: Analysis of a boundary layer separation over a bump using large eddy simulation. In: AIAA paper 2001-2558, 15th AIAA CFD Conference, Anaheim, CA, 2001
    • (2001) 15th AIAA CFD Conference
    • Arad, E.1
  • 4
    • 0036642235 scopus 로고    scopus 로고
    • Active control of separated flow on a wall-mounted "Hump" at high Reynolds numbers
    • July
    • Seifert, A., Pack, L.G.: Active control of separated flow on a wall-mounted "Hump" at high Reynolds numbers. AIAA J., 40(7), 1363-1372 (2002) (July)
    • (2002) AIAA J , vol.40 , Issue.7 , pp. 1363-1372
    • Seifert, A.1    Pack, L.G.2
  • 5
    • 34250810109 scopus 로고    scopus 로고
    • Arad, E., Martin, P.B., Wilson, J., Tung C.: Control of massive separation on a thick-airfoil wing: a computational and experimental study. In: AIAA paper 2006-0332, Reno NV, January 2006
    • Arad, E., Martin, P.B., Wilson, J., Tung C.: Control of massive separation on a thick-airfoil wing: a computational and experimental study. In: AIAA paper 2006-0332, Reno NV, January 2006
  • 6
    • 0020902871 scopus 로고
    • Influence of base slant on the wake structure and drag of road vehicles
    • Ahmed, S.R.: Influence of base slant on the wake structure and drag of road vehicles. J. Fluids Eng. 105, 429-434 (1983)
    • (1983) J. Fluids Eng , vol.105 , pp. 429-434
    • Ahmed, S.R.1
  • 7
    • 85072351804 scopus 로고
    • Some salient features of the time-averaged ground vehicle wake. SAE Tech. Pap
    • 840300:2
    • Ahmed, S.R., Ramm, G., Faltin, G.: Some salient features of the time-averaged ground vehicle wake. SAE Tech. Pap. Ser. 93(840300:2), 473-503 (1984)
    • (1984) Ser , vol.93 , pp. 473-503
    • Ahmed, S.R.1    Ramm, G.2    Faltin, G.3
  • 8
    • 0029158855 scopus 로고
    • 2 model
    • 2 model. AIAA J. 33(4), 659-664 (1995)
    • (1995) AIAA J , vol.33 , Issue.4 , pp. 659-664
    • Durbin, P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.