An accurate method for evaluating the derivatives along circular paths on the surface is proposed. Calculations are made on various practical configurations such as wing-body combinations, tandem wings, wings with the dihedral angles at sideslip, ground effects, interference between a sphere and wind-tunnel etc. Comparisons with experiments show good agreement.
Finite Element Calculations for Aerodynamic Coefficients of 3-Dimensional Body in Subsonic Flow Using Green's Function Method
1982
29 pages
Report
No indication
English
Aerodynamic coefficients of oscillating airfoil in two-dimensional subsonic flow
Engineering Index Backfile | 1951
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