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
Librarian view | Catkey: 3157939