SUPERSONIC TRANSPORT PHASE 3 PROGRAM. VOLUME 3-TECHNICAL/ENGINE. B. ENGINE DESIGN REPORT. PART I-MAJOR COMPONENTS

Abstract

Contents: Compressors; Primary combustor; Turbine, Augmentor, Exhaust nozzle and thrust reverser; Augmentor and exhaust nozzle cooling; Main seals and bearings; Accessory drives; Frames and structures.

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Document Details

Document Type
Technical Report
Publication Date
Sep 06, 1966
Accession Number
AD0378484

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Engineered Resilient Systems
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Creep
  • Engineers
  • Failure Mode And Effect Analysis
  • Fasteners
  • Friction
  • Gas Turbines
  • Geometry
  • Heat Transfer
  • Joining
  • Joints
  • Mechanical Working
  • Mechanics
  • Pressure Distribution
  • Test And Evaluation
  • Test Facilities
  • Turbine Components

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics