SUPERSONIC TRANSPORT PROGRAM. PHASE II-C REPORT. AIR INDUCTION SUBSYSTEM SPECIFICATION. SST BOEING MODEL 2707.

Abstract

This specification establishes the requirements for performance, design, test and qualification of the Air Induction Subsystem. This subsystem shall provide the engine with the quantity of air demanded within the flow distortion limits of the engine. This subsystem requires a control subsystem and an anti-icing subsystem, and provides for high pressure recovery within the flow. The installation of the subsystem is defined by the Aircraft Engine Installation Subsystem Specification (D6A10113-1).

Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1966
Accession Number
AD0805655

Entities

People

  • R. E. Ensley

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Engines
  • Aircrafts
  • Distortion
  • Engines
  • High Pressure
  • Qualifications
  • Recovery
  • Specifications
  • Supersonic Transport Aircraft
  • Transport Ships
  • Vehicles

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.
  • Software Engineering

Technology Areas

  • Hypersonics