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About Fatigue Evaluation of Wing and Associated Structure on Small Airplanes
P0110106». Organisation Name pad Addie". Airframe Branch aircraft and usage. Methods for evaluating the wing and associated structure for fatigue underethe . A large stress change, which causes fatigue damage, occurs once
Detailed Information
| Author: | Unknown |
|---|---|
| Publication Year: | 2002 |
| Pages: | 42 |
| Language: | English |
| File Size: | 2.35 |
| Format: | |
| Price: | FREE |
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