Author | : John C. Martin |
Publisher | : |
Total Pages | : 720 |
Release | : 1954 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
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.