Correlation of the vortex lattice method on rotor/wing configurations.
LIU, D. T. /HUGHES TOOL CO., AIRCRAFT DIV., STABILITY AND CONTROL SECTION, CULVER CITY, CALIFORNIA,, RODDEN, W. P.
Journal of Aircraft ; 6 , 4 ; 375
1969
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Experimental and Nonlinear Vortex Lattice Method Results for Various Wing-Canard Configurations
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