Length-to-Depth Ratio Effects on Aerodynamic Surface Quantities of a Hypersonic Gap Flow
Author:
Affiliation:
1. National Institute for Space Research, 12630-000 São Paulo, Brazil
Funder
Conselho Nacional de Desenvolvimento Científico e Tecnológico
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055826
Reference29 articles.
1. Surface Step Induced Gap Heating in the Shuttle Thermal Protection System
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5. Aerodynamic Heat Transfer to RSI Tile Surfaces and Gap Intersections
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