Accession Number : AD0478759


Title :   PRELIMINARY TEST PLAN OF THE SST INLET/GE4/J5G 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 : 31


Abstract : A preliminary plan outlining the test program for the full scale SST inlet and controller with the GE4/J5G engine is presented in this document. 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 are (1) testing of the full scale SST inlet and 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 , WIND TUNNEL MODELS , MODEL TESTS , SUPERSONIC CHARACTERISTICS , SCHEDULING , CONTROL SYSTEMS , MANAGEMENT PLANNING AND CONTROL , PERFORMANCE(ENGINEERING) , SUBSONIC CHARACTERISTICS , SIMULATION , TURBOJET EXHAUST NOZZLES , JET TRANSPORT AIRCRAFT , WINGS , FLUID FLOW , ANGLE OF ATTACK , ENGINEERING DRAWINGS , INSTRUMENTATION , DATA PROCESSING , DIGITAL COMPUTERS , PROGRAMMING LANGUAGES , TRANSONIC CHARACTERISTICS


Subject Categories : Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE