Download Coupled Rotor/Fuselage Dynamic Analysis of the AH-1G Helicopter and Correlation with Flight ... PDF Free - Full Version
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About Coupled Rotor/Fuselage Dynamic Analysis of the AH-1G Helicopter and Correlation with Flight ...
A NASTRAN finite element method is used to form isolated fuselage modal characteristics. C81 is then used to couple the rotor and airframe.
Detailed Information
| Author: | Unknown |
|---|---|
| Publication Year: | 2015 |
| Pages: | 154 |
| Language: | English |
| File Size: | 2.72 |
| Format: | |
| Price: | FREE |
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