Accession Number : AD0377691

Title :   DEVELOPMENT OF A SUPERSONIC TRANSPORT AIRCRAFT ENGINE PHASE II-C.

Descriptive Note : Monthly progress rept. no. 15, 1-30 Sep 66.

Corporate Author : PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FLA FLORIDA RESEARCH AND DEVELOPMENT CENTER

Report Date : 10 OCT 1966

Pagination or Media Count : 178

Descriptors :   (*TURBOFAN ENGINES, SUPERSONIC AIRCRAFT), (*JET TRANSPORT PLANES, SUPERSONIC AIRCRAFT), COMPATIBILITY, MAINTAINABILITY, VALUE ENGINEERING, QUALITY CONTROL, RELIABILITY (U) AXIAL FLOW COMPRESSORS, COMBUSTION CHAMBERS, AXIAL FLOW TURBINES, BEARINGS, SEALS, JET ENGINE FUELS, JET ENGINE NOISE, FUEL CONSUMPTION, AXIAL FLOW COMPRESSOR BLADES, PERFORMANCE(ENGINEERING), TURBINE BLADES, DAMAGE, FUEL NOZZLES, PARTIAL DIFFERENTIAL EQUATIONS, JET ENGINE INLETS

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE