Accession Number : AD0376666

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

Descriptive Note : Monthly progress rept. no. 5, 1-30 Nov 65.

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

Report Date : 10 DEC 1965

Pagination or Media Count : 79

Descriptors :   (*JET TRANSPORT PLANES, *TURBOFAN ENGINES), (*SUPERSONIC AIRCRAFT, TURBOFAN ENGINES), DESIGN, CONSTRUCTION, AXIAL FLOW FANS, AXIAL FLOW COMPRESSORS, COMBUSTION CHAMBERS, AXIAL FLOW TURBINES, TURBINE BLADES, FILM COOLING, HEAT TRANSFER, CASCADE STRUCTURES, TURBOJET INLETS, DUCT INLETS, TURBOJET EXHAUST NOZZLES, THRUST REVERSAL, VARIABLE AREA NOZZLES, BLEED SYSTEMS, THRUST AUGMENTOR NOZZLES, MODEL TESTS, PERFORMANCE(ENGINEERING)

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE