Accession Number : AD0378490

Title :   SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III PROPOSAL. BOEING MODEL 2707. COORDINATED INLET/ENGINE TEST PLAN (GENERAL ELECTRIC).

Corporate Author : BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV

Report Date : 06 SEP 1966

Pagination or Media Count : 30

Abstract : A preliminary plan outlining the test program for the full-scale SST inlet and controller with the GE4/J5P engine is presented in this document. This plan will be prepared in greater detail as the B-2707 Program advances. The over-all scope of the test consists of the following two major test programs: Testing in the full-scale SST inlet and controller without the engine in the supersonic tunnel, and Testing the full-scale inlet/engine combination with flight-type inlet and engine control systems in the supersonic and transonic tunnels simulating, to the maximum degree possible, the B-2707 flight envelope.

Descriptors :   (*JET TRANSPORT PLANES, TURBOJET INLETS), (*TURBOJET ENGINES, JET TRANSPORT PLANES), SUPERSONIC AIRCRAFT, WIND TUNNEL MODELS, TEST METHODS, INSTALLATION, ENGINE AIR SYSTEMS COMPONENTS, BLEED SYSTEMS, AFTERBURNERS, ENGINE STARTERS, AERODYNAMIC CHARACTERISTICS, TRANSONIC CHARACTERISTICS, SUPERSONIC CHARACTERISTICS, TEST EQUIPMENT

Subject Categories : Transport Aircraft
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE