Performance Of A Variable Divergent Shroud Ejector Nozzle Designed For Flight Mach Numbers Up To 3 0
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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
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
language: en
Publisher:
Release Date: 1966