Development of a stagnation temperature probe for supersonic combustion flows
Source abstract
Abstract
As part of the French hypersonic programme (PREPHA), a probe has been developed to measure the stagnation temperature in an air/hydrogen supersonic combustion ramjet engine (SCRAMJET)
Only a short abstract or summary was supplied by the source.
Source: openalex_inverted_index · Quality: short
Research context
OpenAlex topics: Rocket and propulsion systems research · Gas Dynamics and Kinetic Theory · Computational Fluid Dynamics and Aerodynamics
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References
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