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Strain gage attachment by spot welding reduces the fatigue strength of ti-6al-4v, rene 41, and inconel x
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Imig, L. A. |
| Copyright Year | 1972 |
| Description | Fatigue tests were conducted with constant-amplitude axial stresses in the ratio of minimum to maximum stress of 0.05 (R=0.05). Specimens with and without strain gages were tested at 21 C, and superalloy specimens with and without strain gages were tested at 21 C and 815 C. |
| File Size | 105699 |
| File Format | |
| Language | English |
| Publisher Date | 1972-07-01 |
| Access Restriction | Open |
| Subject Keyword | Materials Axial Stress Spot Welds Gold Alloys Weld Strength Rene 41 Aluminum Alloys Strain Gages Metal Foils Stainless Steels Stress Ratio Inconel Trademark Fatigue Tests Titanium Alloys Heat Resistant Alloys Fatigue Materials Backups Room Temperature Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |