Flutter analysis of a wraparound fin projectile considering rolling motion

Journal of Spacecraft and Rockets

Volumn 39, Issue 1, 2002, Pages 66-72

  Paek, Seung Kil ^a,b   Bae, Jae Sung ^a   Lee, In ^a  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^b Korea Aerospace Industries Inc   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

NAVIER STOKES EQUATIONS; PROJECTILES;

AEROELASTIC STABILITY; ROLLING MOTION;

FLUTTER (AERODYNAMICS);

EID: 0036192358     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3783     Document Type: Article

References (12)

1. Subsonic and transonic aerodynamics of a wraparound fin configuration
2. Computation of roll moment for projectile with wraparound fins using Euler equations
3. Multiple-zone strategy for supersonic missiles
4. Analysis of missile configurations with wrap-around fins using computational fluid dynamics
5. Nonlinear aerodynamics of bodies in coning motion
6. Aeroelastic effects on the roll characteristics of a wraparound fin projectile
7. Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at mach number of 0.7
8. Static aeroelastic analysis for wrap-around fins of a rolling projectile
9. A diagonal form of an implicit approximate factorization algorithm
10. Computation of the roll moment for a projectile with wrap-around fins