Accession Number : AD0478760


Title :   PRELIMINARY TEST PLAN OF THE SST INLET/JTF 17A-20B ENGINE SYSTEM - AEDC.COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C REPORT.


Corporate Author : BOEING CO RENTON WA


Report Date : 01 Jan 1966


Pagination or Media Count : 34


Abstract : A preliminary plan outlining the test program for the full scale SST inlet and controller with the JTF17A-20B engine is presented. This plan will be prepared in greater detail as the SST program advances. The overall scope of the test consists of two major test programs: (1) testing of the full scale SST inlet and inlet controller without the engine in the supersonic tunnel at Arnold Engineering Development Center (AEDC); (2) testing of the full scale inlet/engine combination with flight type inlet and engine control systems in the AEDC supersonic and transonic tunnels simulating to the maximum degree possible the SST flight envelope. (Author)


Descriptors :   *TURBOJET INLETS , *TURBOFAN ENGINES , SUPERSONIC AIRCRAFT , SUPERSONIC CHARACTERISTICS , TRANSONIC CHARACTERISTICS , CONTROL SYSTEMS , SCHEDULING , MANAGEMENT PLANNING AND CONTROL , MODEL TESTS , WIND TUNNEL MODELS , SIMULATION , FLIGHT TESTING , PERFORMANCE(ENGINEERING) , COMPATIBILITY , STAGNATION POINT , TRANSPORT AIRCRAFT , EXHAUST NOZZLES , WINGS , PITCH(MOTION) , YAW , FLUID FLOW , ANGLE OF ATTACK , JET ENGINE NACELLES , INSTRUMENTATION , DATA PROCESSING , DIGITAL COMPUTERS , COMPUTER PROGRAMMING , PROGRAMMING LANGUAGES


Subject Categories : Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE