Study is part of program to study aspects of jet interference; variables involved were nozzle configuration and position beneath wing, and pressure ratio; design procedure for rockets used is given; incremental normal force due to jet interference on wing varied from one to 2 times rocket thrust and generally decreased as pressure ratio increased.
Pressure loads produced on flat-plate wing by rocket jets exhausting in spanwise direction below wing and perpendicular to free-stream flow of mach number 2.0
NASA -- Tech Note
1961
47 pages
Report
English
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