Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle designed for flight Mach numbers to 3.0
Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0
01.01.1961
Report
Keine Angabe
Englisch
Internal-performance of two-position divergent shroud ejector
Engineering Index Backfile | 1961
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