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:

1968-04-10

Pagination or Media Count:

35.0

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