Accession Number : AD0866590

Title :   Design and Evaluation of a High Temperature Radial Turbine.

Descriptive Note : Quarterly technical summary rept. no. 10, 1 Nov 69-31 Jan 70,

Corporate Author : PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FL FLORIDA RESEARCH AND DEVELOPMEN T CENTER

Personal Author(s) : Calvert, G. S.

Report Date : 18 FEB 1970

Pagination or Media Count : 18

Abstract : Detailed performance predictions are presented. The second and third nozzle castings were received for evaluation, and the first bicast rotor for destructive spin-test was delivered. The replacement test rotor was machined, balanced, spin-tested, and used in the assembly of Turbine Build One. The rig was mounted on the test stand and cold flow testing was completed. (Author)

Descriptors :   (*GAS TURBINES, DESIGN), GAS TURBINE NOZZLES, CASTINGS, GAS TURBINE ROTORS, TESTS, PERFORMANCE(ENGINEERING).

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE