Lifting-surface theory for V/STOL aircraft in transition and cruise. II
暂无分享,去创建一个
[1] N. Ellis. Theory and computer study of a wing in a slipstream , 1966 .
[2] C. Koning,et al. Influence of the Propeller on Other Parts of the Airplane Structure , 1935 .
[3] J Stuper. Effect of propeller slipstream on wing and tail , 1938 .
[4] Marc E. Brenckmann,et al. Experimental investigation of the aerodynamics of a wing in a slipstream , 1957 .
[5] Abe Silverstein,et al. Design Charts for Predicting Downwash Angles and Wake Characteristics Behind Plain and Flapped Wings , 1939 .
[6] K. W. Goodson. Longitudinal aerodynamic characteristics of a flapped tilt-wing four-propeller V/STOL TRANSPORT model , 1966 .
[7] Richard E Kuhn,et al. Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees , 1956 .
[8] E. S. Levinsky,et al. LIFTING SURFACE THEORY AND TAIL DOWNWASH CALCULATIONS FOR V/STOL AIRCRAFT IN TRANSITION AND CRUISE , 1968 .
[9] W. L. Gray,et al. A Method for Calculating the Subsonic Steady-State Loading on an Airplane With a Wing of Arbitrary Plan Form and Stiffness , 1953 .
[10] H. H. Heyson,et al. Induced Velocities Near a Lifting Rotor with Nonuniform Disk Loading , 1957 .
[11] E Kisielowski,et al. INVESTIGATION OF PROPELLER SLIPSTREAM EFFECTS ON WING PERFORMANCE , 1967 .
[12] I. H. Abbott,et al. Theory of Wing Sections , 1959 .
[13] M. Hall,et al. The structure of concentrated vortex cores , 1966 .
[14] H. Glauert. The elements of aerofoil and airscrew theory , 1926 .
[15] F Weinig,et al. The Effect of the Slipstream on an Airplane Wing , 1939 .