Numerical and Experimental Analysis of Capsules Ablation and Shape Change including Heating Transient Effects
Author:
Affiliation:
1. University of Rome "La Sapienza"
2. von Kármán Institute for Fluid Dynamics
Publisher
American Institute of Aeronautics and Astronautics
Reference47 articles.
1. Aerothermal Testing of Space and Missile Materials in the Arnold Engineering Development Center Arc Jet Facilities
2. Characterization of the performance of shock-tube wind tunnels
3. Simeonides, G. “The VKI hypersonic wind tunnels and associated measurement techniques,” Tech. Rep. Memorandum 46, Von Karman Institute for Fluid Dynamics, 1990.
4. Flow characterization and boundary layer transition studies in VKI hypersonic facilities (Invited)
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