Computation of Stability Derivatives of Spinning Missiles Using Unstructured Cartesian Meshes
20th AIAA Applied Aerodynamics Conference ; 2002 ; St. Louis , Missouri
2002-01-01
Conference paper
Electronic Resource
English
Aeroelastic stability of slender, spinning missiles
AIAA | 1992
|Dynamic stability of symmetric spinning missiles.
NTRS | 1968
|Dynamic stability of symmetric spinning missiles.
AIAA | 1968
|Aeroelastic stability of slender, spinning missiles
AIAA | 1989
|