John C. Martin

Percy J. Bobbitt

Margaret S. Diederich

A theoretical investigation is presented of the contribution of horizontal tails to the lift and pitching moment due to angle of attack, a constant rate of pitch, and a constant vertical acceleration. Numerical values of the aerodynamic coefficients associated with these motions are presented for a number of two-dimensional wing-tail combinations, a triangular wing-tail combination, and a number of rectangular-wing - triangular-tail combinations.

A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds

United States. National Advisory Committee for Aeronautics

Harry L. Runyan

John A. Zalovcik

Carl Kaplan

Frank M. Hamaker

George B. Brajnikoff

John M. Riebe

M. M. Frocht

A Method of Calibrating Airspeed Installations on Airplanes at Transonic and Supersonic Speeds by the Use of Accelerometer and Attitude-angle Measurements

John C. Martin

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