An Improved Computational Model for Predicting the Unsteady Aerodynamic Loads of Rotor Blades

By Daughaday H.   Piziali R. A.  

Journal of the American Helicopter Society, Vol. 11, Iss. 4, 1966-10 ,pp. : 3-10

AHS International

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Development and Test of the BO 105 Rigid Rotor Helicopter

By Weiland Emil F.  

Journal of the American Helicopter Society, Vol. 14, Iss. 1, 1969-01 ,pp. : 22-37

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Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO 105 Coupled Rotor/Fuselage Dynamics

By Tischler Mark B.   Cauffman Mavis G.  

Journal of the American Helicopter Society, Vol. 37, Iss. 3, 1992-07 ,pp. : 3-17

AHS International

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Prediction of Dynamic Stall and Unsteady Airloads for Rotor Blades

By Gangwani Santu T.  

Journal of the American Helicopter Society, Vol. 27, Iss. 4, 1982-10 ,pp. : 57-64

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Rotor unsteady aerodynamics model using an efficient free-vortex method

By Li Pan   Chen Renliang  

Aircraft Engineering, Vol. 84, Iss. 5, 2012-08 ,pp. : 311-320

Emerald Group Publishing Ltd

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