THE INFLUENCE OF AERODYNAMIC HEATING ON THE STRUCTURAL DESIGN OF HIGH-SPEED AIRCRAFT. PART 9. DEVELOPMENT OF STRUCTURAL DESIGN CRITERIA FOR AIRCRAFT SUBJECTED TO AERODYNAMIC HEATING

Abstract

The influence of aerodynamic heating on the structural strength, stiffness and life design of high-speed aircraft is discussed. Critical design conditions are suggested for the strength and stiffness design OF AIRFRAMES EXPERIENCING ELEVATED TEMPERATURES. Fatigue and creep design specifications are discussed. Safety factor requirements are recommended.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1960
Accession Number
AD0264131

Entities

People

  • John W. Leech
  • Warren L. Mccabe

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Airplanes
  • Atmospheric Motion
  • Boundary Layer
  • Gust Loads
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • Mach Number
  • Materials
  • Mechanical Properties
  • Mechanics
  • Probability Distributions
  • Random Variables
  • Sea Level
  • Temperature Gradients

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerospace Engineering
  • Mechanical Engineering/Mechanics of Materials.