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Volumn 113, Issue 1139, 2009, Pages 9-20

Experimental investigation of the aerodynamic characteristics of generic fan-in-wing configurations

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; FIGHTER AIRCRAFT; FLOW VISUALIZATION; GROUND EFFECT; JET FLAPS; VELOCITY MEASUREMENT; WIND TUNNELS;

EID: 60349125721     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000002736     Document Type: Article
Times cited : (10)

References (18)
  • 4
    • 85036890358 scopus 로고    scopus 로고
    • HALL, L.P., HICKEY, D.H. and KIRK IV. Aerodynamic characteristics of a full-scale fan-in-wing taodel including results in ground effect with nosefan pitch control, USA, NASA-TC-D-2368, 1964.
    • HALL, L.P., HICKEY, D.H. and KIRK IV. Aerodynamic characteristics of a full-scale fan-in-wing taodel including results in ground effect with nosefan pitch control, USA, NASA-TC-D-2368, 1964.
  • 5
    • 85036886851 scopus 로고    scopus 로고
    • KIKBY, R.H. and CHAMBERS, J.R. Flight investigation of dynamic stability and control characteristics of a 0.18-scale model of a fan-in-wfeg VTOL airplane, NASA-TN-D-3412, USA, 1966.
    • KIKBY, R.H. and CHAMBERS, J.R. Flight investigation of dynamic stability and control characteristics of a 0.18-scale model of a fan-in-wfeg VTOL airplane, NASA-TN-D-3412, USA, 1966.
  • 6
    • 85036873240 scopus 로고    scopus 로고
    • OBERTO, R.J., RENSELAKR D.J. and ALFANO, D.L. Analysis of performance characteristics in ground effect of a large scale V STOL multi-fanin-wing transport model, NASA-CR-1180, USA, 1968.
    • OBERTO, R.J., RENSELAKR D.J. and ALFANO, D.L. Analysis of performance characteristics in ground effect of a large scale V STOL multi-fanin-wing transport model, NASA-CR-1180, USA, 1968.
  • 8
    • 85036882646 scopus 로고    scopus 로고
    • WILSON, J.C, GENTRY, G.L. and GORTON S.A. wind tunnel test results of a 1/8-scale model, NASA TM-4710, USA, 1996.
    • WILSON, J.C, GENTRY, G.L. and GORTON S.A. wind tunnel test results of a 1/8-scale model, NASA TM-4710, USA, 1996.
  • 10
    • 85003393505 scopus 로고
    • Experimental investigation of flow distortion in fan-in-wing inlets
    • SCHAUB, U. W. Experimental investigation of flow distortion in fan-in-wing inlets, JAircr, 1968, 5, (5), pp 473-478.
    • (1968) JAircr , vol.5 , Issue.5 , pp. 473-478
    • SCHAUB, U.W.1
  • 11
    • 60349106807 scopus 로고
    • Aerodynamic characteristics of large-scale model with a lift fan mounted in a 5-percent-thick triangular wing, including the effects of BLC on the lift-fan-inlet
    • HODDER, B.K., KIRK, J.V. and HALL, L.P. Aerodynamic characteristics of large-scale model with a lift fan mounted in a 5-percent-thick triangular wing, including the effects of BLC on the lift-fan-inlet, NASA TN D-7031, 1970.
    • (1970) NASA TN , vol.D-7031
    • HODDER, B.K.1    KIRK, J.V.2    HALL, L.P.3
  • 12
    • 85003297722 scopus 로고
    • Performance characteristics of a model VTOL lift fan in crossflow
    • LIEBLEIN, S., YUSKA, JA. and DIEDRICH, J.H.. Performance characteristics of a model VTOL lift fan in crossflow, JAircr, 10, (3), 1973, pp 131-136.
    • (1973) JAircr , vol.10 , Issue.3 , pp. 131-136
    • LIEBLEIN, S.1    YUSKA, J.A.2    DIEDRICH, J.H.3
  • 13
    • 60349130563 scopus 로고
    • Aerodynamics of V/STOL aircraft powered by lift fans
    • September
    • HICKEY, D.H. and COOK, W.L. Aerodynamics of V/STOL aircraft powered by lift fans, AGARD CP 22, (15), September 1967.
    • (1967) AGARD CP , vol.22 , Issue.15
    • HICKEY, D.H.1    COOK, W.L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.