Accession Number:

AD0478759

Title:

PRELIMINARY TEST PLAN OF THE SST INLET/GE4/J5G ENGINE SYSTEM - AEDC. COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C REPORT.

Descriptive Note:

Corporate Author:

BOEING CO RENTON WA

Personal Author(s):

Report Date:

1966-01-01

Pagination or Media Count:

31.0

Abstract:

A preliminary plan outlining the test program for the full scale SST inlet and controller with the GE4J5G 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 inletengine 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