SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III PROPOSAL. BOEING MODEL 2707. VOLUME II-9. AIRFRAME DESIGN REPORT. PART E. STRUCTURAL TESTS

Abstract

A comprehensive development and verification test program has been established for the structure of the B-2707 airplane. It recognizes the more demanding usage and environment to which the airplane is subjected, and the use of relatively new structural materials and processes. Additionally, it recognizes the problems of contemporary airplanes and provides testing of proper magnitude and timing to preclude recurrence of similar problems on the SST. Structural areas of concern have been covered by systematic development tests to provide the maximum information possible prior to final design. Toward this end, Boeing has conducted development tests of the SST structure and materials to establish reliable strength, fatigue life, and fail-safe concepts continuously during the past 8-years.

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Document Details

Document Type
Technical Report
Publication Date
Sep 06, 1966
Accession Number
AD0804730

Entities

People

  • D. R. Donaldson

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircrafts
  • Airframes
  • Control Surfaces
  • Fatigue Tests (Mechanics)
  • Fuselages
  • Geometry
  • High Lift Devices
  • Honeycomb Structures
  • Manufacturing
  • Materials
  • Mechanical Working
  • Mechanics
  • Spars
  • Test And Evaluation
  • Test Facilities
  • Test Methods

Readers

  • Joint Military Operations and Doctrine.
  • Software Engineering

Technology Areas

  • Hypersonics