论文信息 - Analysis of Aeroelastic Stability of a Slender Launch Vehicle Using Aerodynamic Data - 字舞流文

Analysis of Aeroelastic Stability of a Slender Launch Vehicle Using Aerodynamic Data

R. Pandiyan | Manish Trikha | Debiprosad Roy Mahapatra | Srinivasan Gopalakrishnan | S. Gopalakrishnan | M. Trikha | D. Mahapatra | R. Pandiyan

[1] Dewey H. Hodges,et al. Introduction to Structural Dynamics and Aeroelasticity , 2002 .

[2] J. W. Cornelisse,et al. Rocket propulsion and spaceflight dynamics , 1979 .

[3] R. L. Baker,et al. Launch Vehicle Self-Sustained Oscillation from Aeroelastic Coupling Part 1: Theory , 1998 .

[4] H. Julian Allen,et al. A study of effects of viscosity on flow over slender inclined bodies of revolution , 1951 .

[5] L. E. Ericsson,et al. Aeroelastic Vehicle Dynamics of a Proposed Delta II 7920-10L Launch Vehicle , 2000 .

[6] C. D. Mote,et al. Current Research on the Vibration and Stability of Axially-Moving Materials , 1988 .

[7] J. P. Reding,et al. Fluid dynamics of unsteady separated flow. Part I. Bodies of revolution , 1986 .

[8] Dewey H. Hodges,et al. Introduction to Structural Dynamics and Aeroelasticity: Contents , 2002 .