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

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)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1966
Accession Number
AD0478760

Entities

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Control Systems
  • Control Systems Engineering
  • Engineering
  • Interdisciplinary Science
  • Supersonic Transport Aircraft
  • Systems Engineering
  • Systems Science
  • Transport Ships
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow