Quantification of condition indicator performance on a split torque gearbox.
- Published in:
- Journal of Intelligent Manufacturing, 2012, v. 23, n. 2, p. 213, doi. 10.1007/s10845-009-0346-y
- By:
- Publication type:
- Article
Works matching DE "HELICOPTERS -- Parts"
Results: 6
1
2
Torsional vibration dynamic analysis of the test rig for intersecting axes gears of helicopters.
- Published in:
- Noise & Vibration Worldwide, 2011, v. 42, n. 11, p. 3, doi. 10.1260/0957-4565.42.11.3
- By:
- Publication type:
- Article
3
Aerodynamic Shape Optimization in Aeronautics: A Fast and Effective Multi-Objective Approach.
- Published in:
- Archives of Computational Methods in Engineering, 2014, v. 21, n. 3, p. 189, doi. 10.1007/s11831-014-9123-y
- By:
- Publication type:
- Article
4
Retardation effects due to overloads in aluminium-alloy aeronautical components.
- Published in:
- Fatigue & Fracture of Engineering Materials & Structures, 2017, v. 40, n. 9, p. 1484, doi. 10.1111/ffe.12591
- By:
- Publication type:
- Article
5
REDUCTION OF THE VIBRATION IN A HELICOPTER BLADE USING PIEZOELECTRIC ACTUATORS.
- Published in:
- Aviation (1648-7788), 2006, v. 10, n. 2, p. 3, doi. 10.3846/16487788.2006.9635927
- By:
- Publication type:
- Article
6
OSVRT NA PROJEKTOVANJE GLAVNOG ROTORA HELIKOPTERA.
- Published in:
- Military Technical Courier / Vojnotehnicki Glasnik, 2015, v. 63, n. 2, p. 87, doi. 10.5937/vojtehg63-6326
- By:
- Publication type:
- Article