Continuous Aerodynamic Modelling of Entry Shapes
Author:
Affiliation:
1. Delft University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6575
Reference28 articles.
1. Shape Optimization for a Small Experimental Re-entry Module
2. Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles
3. 5Craidon, C. “A Description of the Langley Wireframe Geometry Standard (LaWGS) Format,” Tech. Rep. TM 85767, NASA, 1985.
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