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Investigations of cemented and detachable joints of fiber reinforced plastics
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Althof, W. Mueller, J. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1971 |
| Abstract | LAMINATED STRUCTURES OF PLASTICS REINFORCED WITH CARBON AND BORON FIBERS AND CONTAINING BOLT HOLES WERE TESTED FOR STRENGTH UNDER DIFFERENT CONDITIONS OF FIBER ORIENTATION, HOLE DIAMETER, AND HOLE SPACING FROM THE EDGES. LAMINATES WITH FIBER ORIENTATIONS IN 0 AND PLUS OR MINUS 45 DEG REACH A RELATIVELY HIGH BOLT HOLE STRENGTH EVEN WITH RELATIVELY SMALL END SPACING AND SHOULD BE PREFERRED FOR AIRCRAFT CONSTRUCTION. A LARGE NUMBER OF PRACTICAL ADHESIVES ARE SUITABLE FOR BONDING BORON FIBER REINFORCED PLASTIC LAMINATES TO THEMSELVES OR TO STEEL AND TITANIUM SHEETING. DEFORMABLE HIGH STRENGTH ADHESIVES GAVE THE HIGHEST BOND STRENGTHS. |
| File Size | 830542 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19720004865 |
| Archival Resource Key | ark:/13960/t7mp5rp9h |
| Language | English |
| Publisher Date | 1971-12-01 |
| Access Restriction | Open |
| Subject Keyword | Geomagnetism Pioneer 7 Space Probe Solar Rotation Graphs (charts) Magnetic Fields Solar Wind Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
