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Investigation of the Compressive, Bearing and Shear Creep-Rupture Properties of Aircraft Structural Metals and Joints at Elevated Temperatures.


AD155570

Publication Date 1958
Page Count 10
Abstract No abstract available.
Keywords
  • Airframes
  • Metals
  • Riveted joints
  • Creep
  • Mechanical properties
  • Rupture
  • Shear stresses
  • Stresses
  • Temperature
  • Tensile properties
Source Agency
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
Corporate Authors Cornell Aeronautical Lab., Inc., Buffalo, NY.
Document Type Technical Report
NTIS Issue Number 198101
Contract Number
  • AF33 616 3456
Investigation of the Compressive, Bearing and Shear Creep-Rupture Properties of Aircraft Structural Metals and Joints at Elevated Temperatures.
Investigation of the Compressive, Bearing and Shear Creep-Rupture Properties of Aircraft Structural Metals and Joints at Elevated Temperatures.
AD155570

  • Airframes
  • Metals
  • Riveted joints
  • Creep
  • Mechanical properties
  • Rupture
  • Shear stresses
  • Stresses
  • Temperature
  • Tensile properties
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
  • AF33 616 3456
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