Optimum placement of sensors for vibration measurements on turbine engine blades-Reference-Cited by-同舟云学术

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Optimum placement of sensors for vibration measurements on turbine engine blades

Published:1998-04-20 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit
language:
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Author:

Sensmeier M.¹,Nichol K.¹

Affiliation:

1. Sverdrup Technology, Inc., Arnold AFB, TN

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1849

Reference11 articles.

1. SaltLakeCity,UT,April 1996.

2. DYNAMIC STRESS ANALYSIS OF GAS TURBINE ROTOR AIRFOILS USING THERMOELASTIC TECHNIQUES

3. Sensor placement for on-orbit modal identification and correlation of large space structures

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2. Accurate Strain Gauge Limits Through Geometry Mistuning Modeling;Journal of Propulsion and Power;2018-11

3. Assessment of uncertainty in response estimation for turbine engine bladed disks;Journal of Sound and Vibration;2008-11

4. Robust Optimal Positioning of Strain Gages on Blades;Journal of Turbomachinery;2003-01-01

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