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Fastening on the f-14a for cost effective fatigue resistance. [considering variable geometry wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Beal, B. H. |
| Copyright Year | 1972 |
| Description | Cost effectiveness airframe considerations dictated a variable geometry wing design that requires weight optimization, maximum working stress resistance and minimum fatigue concentration factors. The extensive use of titanium structural materials employed electron beam welding methods and interference fit fastening techniques as principle mechanical joining means for economic F-14A production and reliability engineering. |
| File Size | 4488120 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740022842 |
| Archival Resource Key | ark:/13960/t7bs3js19 |
| Language | English |
| Publisher Date | 1972-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Interference Fit Fittings F-14 Aircraft Wings Electron Beam Welding Cost Effectiveness Airframes Production Engineering Metal Joints Titanium Fasteners Variable Geometry Structures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
