SOME PARTICULARITIES CONCERNING THE MOTION OF BODIES OF REVOLUTION’S FLIGHT TRAJECTORY
THIN, CONICAL SHOCK WAVE
The paper presents a contribution to the aerodynamic body of revolution movement trajectories in the thin atmosphere. As a particular case, the paper refers to flying projectiles and missiles, to customize linarite stationary movements around thin bodies of revolution.
Keywords: projectile, missile, speed potential, Mach number, angle of attack, conical shock wave
Cuvinte cheie: proiectil, rachetă, potenţialul vitezelor, numărul Mach, unghi de atac, undă de șoc conică
