Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers [microform]
- Responsibility
- R.J. Boyle and R. Jackson.
- Imprint
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- Physical description
- 1 v.
- Series
- NASA technical memorandum 106956