Busemann inlet for hypersonic speeds.
Author:
Affiliation:
1. McGill University, Montreal, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28649
Reference9 articles.
1. The Determination of the Thermal Structure of a Combustion Wave by Fine Thermocouples.
2. Measurement of temperature profiles through solid-propellant flames using fine thermocouples
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