New Computational Method to Determine Trim Angle of Attack for Reentry Vehicles
Author:
Affiliation:
1. National University of Defense Technology, 410073 Changsha, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.6211
Reference5 articles.
1. 2Guo, Z. "Numerical Simulation Technique Research for Unsteady Multi-Body Flowfield Involving Moving Boundaries," Ph.D. Dissertation,College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha, PRC,June 2002.
2. Considerations on the spring analogy
3. A fast upwind solver for the Euler equations on three-dimensional unstructured meshes
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