16:162:1622:16228:16228
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- backbone-bending-by-aerodynamic-forces.svg
- 2020/06/25 22:46
- 193.8 KB
- blade-tip-clearance-change.svg
- 2020/06/25 22:46
- 15.8 KB
- clearance-changes-by-flight-loads.svg
- 2020/06/25 22:46
- 112.7 KB
- clearance-changes-by-maneuvering-loads.svg
- 2020/06/25 22:46
- 7.3 KB
- compressor-blade-fracture-by-thermal-bending.svg
- 2020/06/25 22:46
- 317.2 KB
- conclusions-from-clearance-shapes.svg
- 2020/06/25 22:46
- 207.5 KB
- deformations-by-g-forces.svg
- 2020/06/25 22:46
- 176.9 KB
- engine-affecting-by-inertia-forces-acceleration.svg
- 2020/06/25 22:46
- 257.7 KB
- engine-position-influences-damages.svg
- 2020/06/25 22:46
- 96.2 KB
- gyroscopic-forces-at-fan-and-low-pressure-shaft.svg
- 2020/06/25 22:46
- 137.9 KB
- gyroscopic-forces-during-military-maneuver.svg
- 2020/06/25 22:46
- 57.6 KB
- high-frequency-vibrations-of-low-pressure-shafts.svg
- 2020/06/25 22:46
- 167.7 KB
- housing-deformations-near-engine-suspension.svg
- 2020/06/25 22:46
- 227.3 KB
- influences-at-tip-clearances.svg
- 2020/06/25 22:46
- 142.2 KB
- leakage-losses-and-rub-wear-behaviour.svg
- 2020/06/25 22:46
- 180.5 KB
- maintaining-tip-clearances.svg
- 2020/06/25 22:46
- 303.7 KB
- problems-by-deformation-of-compressor-housing.svg
- 2020/06/25 22:46
- 132.2 KB
- rotor-axle-offset-and-gyroscopic-forces.svg
- 2020/06/25 22:46
- 158.6 KB
- rotor-bow-thermal-bending-affecting-operation.svg
- 2020/06/25 22:46
- 142.1 KB
- strain-behaviour-of-engine-components.svg
- 2020/06/25 22:46
- 208.3 KB
- tip-clearance-change-after-shut-down.svg
- 2020/06/25 22:46
- 145.1 KB
- tip-clearance-change-by-heat-strain.svg
- 2020/06/25 22:46
- 16.5 KB
- tip-clearance-change-during-operation.svg
- 2020/06/25 22:46
- 98.5 KB
- tip-clearance-change-during-unsteady-operation.svg
- 2020/06/25 22:46
- 194.6 KB
- tip-clearance-changes-at-turbines-and-compressors.svg
- 2020/06/25 22:46
- 721.8 KB
- why-the-shortest-blades-seem-to-rub-first.svg
- 2020/06/25 22:46
- 101.9 KB
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16/162/1622/16228/16228.txt · Last modified: 2021/07/05 12:29 by 127.0.0.1