Calculated Aerodynamic Loadings of M, W, and Delta Wings in Incompressible Flow
Description:
Report presenting the results of theoretical incompressible-flow calculations of the spanwise lift distributions, lift-curve slopes, spanwise centers of pressure, aerodynamic centers, coefficients of damping in roll, rolling-moment coefficients due to aileron deflection, and induced-drag coefficients of twenty M, W, and delta wings.
Date:
August 30, 1951
Creator:
Diederich, Franklin W. & Latham, W. Owen
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department