The effect of inflow models on the predicted response of helicopters

Journal of the American Helicopter Society

Volumn 43, Issue 1, 1998, Pages 25-36

  Uwe, T P Arnold ^a   Keller, Jeffrey D ^b   Curtiss Jr , H C ^b   Reichert, Günther ^c  

^a ZF Luftfahrttechnik   (Germany)

^b PRINCETON UNIVERSITY   (United States)

^c TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; DYNAMIC RESPONSE; FORECASTING; MATHEMATICAL MODELS;

AERODYNAMIC LAG MODEL; AERODYNAMIC PHASE CORRECTION; INFLOW MODEL; NONLINEAR SIMULATION MODEL;

HELICOPTER ROTORS;

EID: 0031700858     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (14)

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9. Curtiss, H.C., "Stability and Control Modeling," Vertica, Vol. 12, (4), 1988.
10. Abbott, W.Y., Benson, J.O., Oliver, R.G., and Williams, R.A., "Validation Flight Test of UH-60A for Rotorcraft Systems Integration Simulator," Final Report USAAEFA Project No. 79-24, Sep 1982.
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13. Curtiss, H.C. and Shupe, N.K., "A Stability and Control Theory for Hingeless Rotors," American Helicopter Society 27th Annual Forum, Washington D.C., May 1971.
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