Accession Number : AD0376673

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

Descriptive Note : Monthly progress rept. no. 14, 1-31 Aug 66.

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

Report Date : 10 SEP 1966

Pagination or Media Count : 162

Abstract : Contents: Engine Design, Engine Test, Compressor, Primary Combustor, Turbine, Augmentor, Exhaust System, Controls, Bearings and Seals, Fuels and Lubricants, Inlet System Compatibility, Noise, Mockups, Coordination, Maintainability, Value Engineering, Configuration Management, Quality Assurance, and Reliability.

Descriptors :   (*JET TRANSPORT PLANES, *TURBOFAN ENGINES), (*SUPERSONIC AIRCRAFT, TURBOFAN ENGINES), DESIGN, CONSTRUCTION, MODEL TESTS, PERFORMANCE(ENGINEERING), AXIAL FLOW COMPRESSORS, AXIAL FLOW TURBINES, COMBUSTION CHAMBERS, TURBOJET EXHAUST NOZZLES, THRUST AUGMENTOR NOZZLES, THRUST REVERSAL, TURBOJET INLETS, COMPATIBILITY, JET ENGINE NOISE, ATTENUATION, LUBRICANTS, JET ENGINE FUELS, FUEL SYSTEMS, BEARINGS, SEALS, TURBINE BLADES, AERODYNAMIC CHARACTERISTICS, CASCADE STRUCTURES, QUALITY CONTROL, FLOWMETERS

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE