Modeling and Analysis of a 6-DOF Flexible Hypersonic Flight Vehicle
Author:
Affiliation:
1. School of Science, Tianjin University of Science and Technology
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/63/4/63_T-19-55/_pdf
Reference27 articles.
1. 1) Mcnamara, J. J. and Friedmann, P. P.: Aeroelastic and Aerothermoelastic Analysis of Hypersonic Vehicles: Current Status and Future Trends, The 48th AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference, Hawaii, USA, 2007. https://doi.org/10.2514/6.2007-2013
2. 2) Chavez, F. R. and Schmidt, D. K.: Analytical Aeropropulsive/Aeroelastic Hypersonic Vehicle Model with Dynamic Analysis, J. Guid. Control Dynam., 17, 6 (1994), pp. 1308–1319.
3. 3) Bolender, M. A. and Doman, D. B.: Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle, J. Spacecraft Rockets, 44, 2 (2007), pp. 374–386.
4. 4) Bolender, M. A., Oppenheimer, M. W., and Doman, D. B.: Effects of Unsteady and Viscous Aerodynamics on the Dynamics of a Flexible Air-Breathing Hypersonic Vehicle, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Hilton Head, USA, 2007. https://doi.org/10.2514/6.2007-6397
5. 5) Oppenheimer, M. W., Skujins, T., Doman, D. B., and Bolender, M. A.: A Flexible Hypersonic Vehicle Model Developed with Piston Theory, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Hilton Head, USA, 2007. https://doi.org/10.2514/6.2007-6396
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