Flame Cutting of Armor: Effect of Flame Cutting on the Edge Condition of Seven 1/2 Inch Thick Experimental High Alloyh Hard Homogeneous Rolled Aircraft Armor Plate Compositions.

Abstract

The object of this study was to determine the maximum hardness developed by flame cutting subject plates at room temperature and at 400 F preheat, and to examine flamecut edges for cracks developed during the cutting operation.

Document Details

Document Type
Technical Report
Publication Date
Dec 07, 1943
Accession Number
ADA954448

Entities

People

  • S. A. Herres

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Armor
  • Armor Plate
  • Hardness
  • Mechanical Properties

Readers

  • Manufacturing Engineering.
  • Metallurgy