Accession Number : AD0370606

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

Descriptive Note : Monthly progress rept. for Aug 64.

Corporate Author : PRATT AND WHITNEY AIRCRAFT EAST HARTFORD CONN

Report Date : 15 SEP 1964

Pagination or Media Count : 18

Descriptors :   (*SUPERSONIC AIRCRAFT, *JET TRANSPORT PLANES) (U) TURBOJET ENGINES, PERFORMANCE(ENGINEERING), TURBOFAN ENGINES, AFTERBURNERS, AIRCRAFT ENGINE DUCTS, JET ENGINE NOISE, NOZZLE GAS FLOW, ANECHOIC CHAMBERS, FUELS, THERMAL STABILITY, COMPRESSORS, DESIGN, VIBRATION, HEAT TRANSFER, STRUCTURES, MATHEMATICAL ANALYSIS, IMPELLERS, COMBUSTION, TEST EQUIPMENT, FATIGUE(MECHANICS), COOLING, AIR, WIND TUNNELS, SUPERSONIC FLOW, TURBOJET INLETS

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE