Methodology for supersonic panel flutter analysis of thermal protection system seals

Journal of Aircraft

Volumn 38, Issue 6, 2001, Pages 1025-1031

  Cheng, G ^a   Mei, C ^a   Chen, R R ^a  

^a OLD DOMINION UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CANTILEVER BEAMS; FLUTTER (AERODYNAMICS); FREQUENCY DOMAIN ANALYSIS; HEAT SHIELDING; NONLINEAR SYSTEMS; SEALS; TIME DOMAIN ANALYSIS;

CANTILEVER BEAM-SPRING MODEL; THERMAL PROTECTION SYSTEM SEALS;

SUPERSONIC AERODYNAMICS;

EID: 0035516999     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2889     Document Type: Article

References (6)

1. Panel flutter: Review of the aeroelastic stability of plates and shells
2. Review of nonlinear panel flutter at supersonic and hypersonic speeds
3. Finite element time domain-modal formulation for nonlinear flutter of composite panels
4. Development of metallic thermal protection systems for the reusable launch vehicle
5. Periodic behavior of impact oscillators: Single degree of freedom and multiple degree of freedom systems, experiment