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Heat transfer in serpentine passages with turbulence promoters
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:83614
Comparison between measured turbine stage performance and the predicted performance using quasi-3D flow and boundary layer analyses
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:83640
Mach number effects on turbine blade transition length prediction
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:208404