Author : Donald E. Coletti
Publisher :
Page : 36 pages
File Size : 47,81 MB
Release : 1955
Category : Aerodynamics, Supersonic
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 580 pages
File Size : 16,13 MB
Release : 1956
Category : Aeronautics
ISBN :
Author : United States. Wright Air Development Division
Publisher :
Page : 1268 pages
File Size : 49,4 MB
Release : 1957
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 818 pages
File Size : 38,80 MB
Release : 1954
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 448 pages
File Size : 24,28 MB
Release : 1960
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 716 pages
File Size : 18,97 MB
Release : 1956
Category : Aeronautics
ISBN :
Author : Ross B. Robinson
Publisher :
Page : 32 pages
File Size : 45,14 MB
Release : 1952
Category : Aerodynamics, Supersonic
ISBN :
Author : Defense Documentation Center (U.S.)
Publisher :
Page : 894 pages
File Size : 42,39 MB
Release : 1960
Category : Industrial arts
ISBN :
Author :
Publisher :
Page : 484 pages
File Size : 29,25 MB
Release : 1989
Category : Aeronautics
ISBN :
Author : John C. Martin
Publisher :
Page : 720 pages
File Size : 16,34 MB
Release : 1954
Category : 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.
