Effect of thickness on the lateral force and yawing moment of a sideslipping delta wing at supersonic speeds

Kenneth Margolis
naca-tn-1798
Jan 1949


Calculations, based on linearized supersonic-flow theory and on the additional assumption that the Mach cones yaw with the wing, are made to determine the effect of thickness on the lateral force and yawing moment of a sideslipping delta wing at supersonic speeds.

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