Accession Number : AD0838779

Title :   PYLON (F111B) THERMAL ANALYSIS.

Descriptive Note : Technical rept.,

Corporate Author : NAVAL AVIONICS FACILITY INDIANAPOLIS IN

Personal Author(s) : Hobson, James E.

Report Date : 10 APR 1968

Pagination or Media Count : 35

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)

Descriptors :   (*SUPERSONIC AIRCRAFT, EXTERNAL STORES), (*EXTERNAL STORES, AERODYNAMIC HEATING), JET FIGHTERS, ELECTRONIC EQUIPMENT, MOUNTING BRACKETS, THERMAL CONDUCTIVITY, THERMAL ANALYSIS, ADIABATIC GAS FLOW, LAMINAR FLOW, TURBULENCE, NAVAL AIRCRAFT, WIRING DIAGRAMS, CURVE FITTING, MATHEMATICAL PREDICTION.

Subject Categories : Attack and Fighter Aircraft
      Thermodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE