The aerodynamic forces acting on a missile in consequence of small perturbations from a prescribed trajectory are calculated on the basis of slender body theory and piston theory is applied, in some detail, to the specific example of Generalized Missile Dynamics Analysis, II Equations of Motion.
Generalized Missile Dynamics Analysis. III. Aerodynamics
1958
2 pages
Report
No indication
English
SLUB | 1988
|NTIS | 1990
NTIS | 1998
NTIS | 1979