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Acemap > Paper > Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0

Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0

1961 
Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle designed for flight Mach numbers to 3.0
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