Accession Number : AD0376662

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

Descriptive Note : Monthly progress rept. no. 1, 1-31 Jul 65.

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

Report Date : 10 AUG 1965

Pagination or Media Count : 26

Descriptors :   (*JET TRANSPORT PLANES, *TURBOFAN ENGINES), (*SUPERSONIC AIRCRAFT, TURBOFAN ENGINES), DESIGN, CONSTRUCTION, AXIAL FLOW FANS, TURBOJET INLETS, DUCT INLETS, COMBUSTION CHAMBERS, AXIAL FLOW COMPRESSORS, AXIAL FLOW TURBINES, SEALS, BEARINGS, BLEED SYSTEMS, FUEL NOZZLES, GEARS, TURBOJET EXHAUST NOZZLES, THRUST REVERSAL, MODEL TESTS, PERFORMANCE(ENGINEERING), TURBINE BLADES, COOLING, CONVECTION(HEAT TRANSFER)

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE