Design parameters for the development of wing test rig for static test experiment / Ramzyzan Ramly … [et_al.]
Airplanes are designed to stay aloft with the help of wings on both sides. In operation at cruising speed, the wings are subjected to load as much as the weight of the whole aircraft. However during manuever, the wings are subjected much higher load and stress and this stress should be sustained by...
| Main Authors: | , , , |
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| Format: | Research Reports |
| Language: | English |
| Published: |
Research Management Institute (RMI)
2010
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| Subjects: | |
| Online Access: | http://ir.uitm.edu.my/id/eprint/27153/ http://ir.uitm.edu.my/id/eprint/27153/1/LP_RAMZYZAN%20RAMLY%20RMI%2010_5.pdf |