AXIAL COMPRESSION TEST - UPPER TORQUE BOX SKIN WHEEL BUMP FAIRING.

Abstract

A 53-010001 wheel bump fairing test panel was subjected to a hot air blast which produced temperatures of 275 to 305F (at the surface), and dynamic pressures of 15 psig. An air blast was directed to the EC 1675 and fiberglass fairing juncture, and to the aluminum-filled fairing compound and the skin juncture. Each juncture was subjected to 25 cycles of combined heating and air blast and cooled to 100F between cycles. No significant damage occurred in either of the areas. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 10, 1964
Accession Number
AD0431865

Entities

Organizations

  • McDonnell Aircraft Corporation

Tags

DTIC Thesaurus Topics

  • Aluminum
  • Compression
  • Dynamic Pressure
  • Elements
  • Fiberglass
  • Group 13 Elements
  • Inorganic Materials
  • Overpressure
  • Static Pressure

Readers

  • Electrical Engineering
  • Internal Combustion Engine (ICE) Technology.
  • Logistics and Supply Chain Management.