Computation of Stability Derivatives of Spinning Missiles Using Unstructured Cartesian Meshes
20th AIAA Applied Aerodynamics Conference ; 2002 ; St. Louis , Missouri
01.01.2002
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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
|