INVESTIGATION OF THE COMPRESSIVE, BEARING, AND SHEAR CREEP-RUPTURE PROPERTIES OF AIRCRAFT STRUCTURAL METALS AND JOINTS AT ELEVATED TEMPERATURES. Period covered January-December 1955
Cornell Aeronautical Lab., Ic., Buffalo. Various aircraft structural alloys have been exposed to a tension, compression, bearing, and shear creep test program to establish their high-temperature creep and rupture properties under the influence of these types of stresses. From results obtained in this investigation, it has been found that the test alloys display creep characteristics under compression, bearing, and shear stresses quite similar to those obtained in tension creep testing. The high-temperature creep and rupture behaviors of the test alloys have been presented in various tabular and chart forms and correlations of compression, bearing, and shear creep vs. tension creep on a stress basis have been made to assist in the assignment of creep stress values to members undergoing creep strain other than tension. (auth)
- Research Organization:
- Cornell Aeronautical Lab., Inc., Buffalo
- DOE Contract Number:
- AF33(616)-190
- NSA Number:
- NSA-12-012414
- OSTI ID:
- 4314740
- Report Number(s):
- WADC-TR-54-270(Pt. 3); AD-1511
- Resource Relation:
- Other Information: Project title: MATERIALS ANALYSIS AND EVALUATION TECHNIQUES. Task title: DESIGN DATA FOR METALS. Orig. Receipt Date: 31-DEC-58
- Country of Publication:
- United States
- Language:
- English
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