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Published in 2025 at "Journal of Spacecraft and Rockets"
DOI: 10.2514/1.a36092
Abstract: This study presents a numerical investigation of wind tunnel installation effects on the exhaust flow for a high-speed system under a blockage ratio of 16.5%. The configuration features a nozzle and a cavity embedded at…
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Keywords:
high speed;
speed;
installation effects;
large blockage ... See more keywords