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Cold and hot flow tests investigate flow separation in rocket nozzles, suggesting criteria for design improvements.
Cold and hot flow tests were conducted to investigate the flow separation in rocket nozzles. The results are presented. A separation data base including a wide range of literature data is established to evaluate the influence of propellant combination and nozzle design on flow separation. As a result a simple separation criteria is suggested.
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Ralf Stark (2005) studied this question.
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