Report presents mathematical model for use in designing rocket-launching stand. Predicts pressure and thermal environment, as well as thermal responses of structures to impinging rocket-exhaust plumes. Enables relatively inexperienced analyst to determine time-varying distributions and absolute levels of pressure and heat loads on structures.
Pressure And Thermal Modeling Of Rocket Launches
NASA Tech Briefs ; 19 , 11
01.11.1995
Sonstige
Keine Angabe
Englisch
Pressure and Thermal Modeling of Rocket Launches
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