Aerodynamic Heating

Abstract

The objective of this MTP is to determine the effect of high temperature and temperature changes, resulting from aerodynamic heating, on the missile skin, structure, and interior components using laboratory methods. Such information is used to determine the adequacy of equipment to meet specified requirements such as the ability to withstand the aerodynamic heating associated with flying a specified trajectory. (Author)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 24, 1967
Accession Number
AD0718560

Entities

Organizations

  • United States Army Test and Evaluation Command

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aerodynamic Heating
  • Boundary Layer
  • Boundary Layer Flow
  • Combustion
  • Flow Fields
  • Heat Energy
  • Heat Exchangers
  • Heat Transfer
  • Heat Transfer Coefficients
  • Mach Number
  • Measurement
  • Pressure Measurement
  • Processing Equipment
  • Strain Gages
  • Test Facilities
  • Thermal Conductivity
  • Turbulent Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Test and Evaluation
  • Thermal Physics or Thermal Science.