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