Partitioned Time-Domain Substructure Coupling Methodology for Efficient Hypersonic Vehicle Simulation
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109-2140
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051614
Reference25 articles.
1. AndersonJ. D.Jr., Hypersonic and High-Temperature Gas Dynamics, AIAA, Reston, VA, 2000, pp. 9–11.
2. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle
3. Analytical aeropropulsive-aeroelastic hypersonic-vehicle model with dynamic analysis
4. BertinJ. J., Hypersonic Aerothermodynamics, AIAA, Reston, VA, 1994, pp. 1–3.
5. Dynamics and control of hypersonic aeropropulsive/aeroelastic vehicles
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