Simulated flight acoustic investigation of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction
Simulated flight acoustic investigation of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction
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- Washington, D.C. National Aeronautics and Space Adminstration 1986
- 413 p.
- NASA CR 4019 : 1986 .
Supersonic jet noise reduction, Mechanically suppressed ejector, Shock cell noise, Variable cycle engine, Treated ejector
LNASA CR 4019 : 1986
Supersonic jet noise reduction, Mechanically suppressed ejector, Shock cell noise, Variable cycle engine, Treated ejector
LNASA CR 4019 : 1986