An empirical separation and side load model to obtain applied aerodynamic loads has been developed based on data obtained from full-scale J-2S (265K-pound-thrust engine with an area ratio of 40:1) engine and model testing. Experimental data include visual observations of the separation patterns that show the dynamic nature of the separation phenomenon. Comparisons between measured and applied side loads are made. Correlations relating the separation location to the applied side loads and the methods used to determine the separation location are given.
Sea level side loads in high-area-ratio rocket engines
Propulsion Conference ; 1973 ; Las Vegas, NV, US
1973-11-01
Conference paper
No indication
English
Sea level side loads in high-area-ratio rocket engines
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