Aeroelastic behavior of a slender body considering free fittings
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/content/pdf/10.1007/s12206-010-0606-y.pdf
Reference7 articles.
1. D. H. Platus, Ballistic Re-Entry Vehicle Dynamics, Journal of Guidance and Control, 5(1) (1982) 4–16.
2. D. H. Platus, Aeroelastic Stability of Slender, Spinning Missiles, Journal of Guidance, Control, and Dynamics, 15(1) (1992) 144–151.
3. K. D. Bilimoria and D. K. Schmidt, Integrated development of the equation of motion for elastic hypersonic elastic vehicles, J. Guidance, Control and Dynamics, 18(1) (1995).
4. B. Newman and D. K. Schmidt, Numerical and Literal Aeroelastic-Vehicle-Model Reduction for Feedback control Synthesis, Journal of Guidance, Control, and Dynamics, 14(5) (1991) 943–953.
5. R. Livneh and D. K. Schmidt, Unified literal approximations for longitudinal dynamics of flexible vehicles, Journal of Guidance, Control, and Dynamics, 18(5) (1995) 1074–1083.
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