Flight data on liquid-filled shell for spin-up instabilities
Abstract
The stability of a spinning projectile can be adversely affected when a liquid payload is present. Due to the impulsive launch of a spin-stabilized projectile, the liquid payload is subjected to unsteady and time-dependent processes. For example, the liquid must adjust to the rapid spin of the projectile casing. This process is normally called liquid spin-up. Typically, the liquid spin-up process encompasses a large portion of the trajectory, and in fact many flight instabilities have occurred during this spin-up time frame. Flight data for spin-up instabilities of 155 mm projectiles are presented and discussed.
- Publication:
-
Atmospheric Flight Mechanics Conference
- Pub Date:
- August 1983
- Bibcode:
- 1983atfm.conf.....D
- Keywords:
-
- Flight Stability Tests;
- Liquid Filled Shells;
- Liquid Sloshing;
- Projectiles;
- Spin Dynamics;
- Flight Tests;
- Viscous Fluids;
- Yaw;
- Astrodynamics