Research Article
Experimental and Computational Modal Analyses for Launch Vehicle Models considering Liquid Propellant and Flange Joints
Table 1
Geometric parameters of flanges (
t).
| Oxidizer tank | Upper flange | 0.010 m | Lower flange | 0.005 m | Center body | Upper flange | 0.005 m | Lower flange | 0.005 m | Fuel tank | Upper flange | 0.005 m | Lower flange | 0.010 m |
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