Hypersonic Boundary-Layer Duplication Methodology Downstream of the Stagnation Point-Reference-Cited by-同舟云学术

Hypersonic Boundary-Layer Duplication Methodology Downstream of the Stagnation Point

Published:2018-11 Issue:6 Volume:55 Page:1393-1400
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Viladegut Alan¹,Durand Jean-Etienne¹,Pinna Fabio¹,Chazot Olivier¹

Affiliation:

1. von Karman Institute for Fluid Dynamics, 1640 Rhode-Saint-Genèse, Belgium

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.A33978

Reference23 articles.

1. Enthalpy Characterization and Assessment of Copper Catalysis Determination in Inductively Coupled Plasma Facility

2. Diffusion effects on the determination of surface catalysis in Inductively Coupled Plasma facility

3. Development of an innovative validation strategy of gas–surface interaction modelling for re-entry applications

4. PaneraiF. “Aerothermochemistry Characterization of Thermal Protection Systems,” Ph.D. Dissertation, von Karman Institute for Fluid Dynamics/Università Degli Studi Di Perugia, Perugia, Italy, 2012.

5. HelberB. “Material Response Characterization of Low Density Ablators in Atmospheric Entry Plasmas,” Ph.D. Dissertation, von Karman Institute for Fluid Dynamics/Vrije Universiteit Brussels (VUB), Brussels, 2016.

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