Search Results
Showing 1 - 10 of 10 results
Search Results
Mixing and noise benefit versus thrust penalty in supersonic jets using impingement tones
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:106583
Computer method for design of acoustic liners for turbofan engines
Joyner Library
- Fed Docs Stacks
Call Number:
ASK AT REFERENCE DESK
Mixing noise reduction for rectangular supersonic jets by nozzle shaping and induced screech mixing
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:106364
Supersonic jets from bevelled rectangular nozzles
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:106403
Enhanced mixing of a rectangular supersonic jet by natural and induced screech
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:106245
Instability modes excited by natural screech tones in a supersonic rectangular jet
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:106409
Development of phased twin flip-flop jets
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:106404