Experimental and Numerical Investigation of Aerothermal Characteristics of Hypersonic Intermediate Experimental Vehicle
Author:
Affiliation:
1. Italian Aerospace Research Center, 81043 Capua, Italy
2. von Kármán Institute for Fluid Dynamics, 1640 Rhode St. Genèse, Belgium
3. Astrium Space Transportation, 78133 Les Mureaux, France
4. ESA/ESTEC, 2200 AG Noordwijk ZH, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.48331
Reference13 articles.
1. The Pre-X atmospheric re-entry experimental lifting body: program status and system synthesis
2. Pandolfi, M., and Borrelli, S. "An Upwind Formulation for the Numerical Prediction of Non Equilibrium Hypersonic Flows," Lecture Notes in Physics, Vol.371, 1990, pp.416-420. doi:10.1007/3-540-53619-1_227
3. CFD rebuilding of USV-DTFT1 vehicle in-flight experiment
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