PYLON (F111B) THERMAL ANALYSIS.

Abstract

This report covers the means of approximating temperatures reached by mounting surfaces inside the pylon of a supersonic aircraft. The solution was determined by making the heat circuits analogous to electrical circuits and solving with an automatic circuit analysis. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 10, 1968
Accession Number
AD0838779

Entities

People

  • James E. Hobson

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Automatic
  • Circuit Analysis
  • Circuits
  • Electrical Circuits
  • Energy
  • Heat Energy
  • Jet Aircraft
  • Supersonic Aircraft
  • Thermal Analysis
  • Vehicles

Readers

  • Aerodynamics/Aeronautics.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Integrated Circuit Design and Technology.

Technology Areas

  • Hypersonics