A Generalization of Effective Mass for Selecting Free–Free Target ModesSource: Journal of Vibration and Acoustics:;2007:;volume( 129 ):;issue: 001::page 121DOI: 10.1115/1.2424980Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: One of the most important tasks in pretest analysis and modal survey planning is the selection of target modes. The target modes are those mode shapes that are determined to be dynamically important using some definition. While there are many measures of dynamic importance, one of the measures that has been of greatest interest to structural dynamicists, is the contribution of each mode to the dynamic loads at an interface. Dynamically important modes contribute significantly to the interface loads and must be retained in any reduced analytical representation. These modes must be identified during a ground vibration test to validate the corresponding finite element model. Structural dynamicists have used interface load based effective mass measures to efficiently identify target modes for constrained structures. The advantage of these measures of dynamic importance is that they are absolute, in contrast to other measures that only indicate the importance of one mode shape relative to another. However, in many situations, especially in aerospace applications, structures must be tested in a free–free configuration. In the case of free–free elastic modes, the effective mass values are zero, making them useless measures of dynamic importance. This paper presents a new effective mass like measure of absolute dynamic importance that can be applied to free–free structures. The new method is derived based upon the free–free modal equations of motion. The approach is shown to be directly related to ranking mode shapes based on approximate balanced singular values. But, unlike the approximate balanced singular value approach, it is an absolute measure of importance. A numerical example of a general spacecraft system is presented to illustrate the application of the new technique. Dynamically important mode shapes were easily identified for modal acceleration, velocity, and displacement output. The new method provides an efficient technique for selecting target modes for a modal vibration test, or the reduction of a modal based analytical model to the dynamically important mode shapes.
keyword(s): Electromagnetic fields , Stress , Displacement , Finite element model , Shapes , Space vehicles , Equations of motion , Enterprise information management , Vibration tests , Degrees of freedom AND Aerospace industry ,
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| contributor author | Daniel C. Kammer | |
| contributor author | Andrew Kostuch | |
| contributor author | Joseph Cessna | |
| date accessioned | 2017-05-09T00:26:27Z | |
| date available | 2017-05-09T00:26:27Z | |
| date copyright | February, 2007 | |
| date issued | 2007 | |
| identifier issn | 1048-9002 | |
| identifier other | JVACEK-28884#121_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/137176 | |
| description abstract | One of the most important tasks in pretest analysis and modal survey planning is the selection of target modes. The target modes are those mode shapes that are determined to be dynamically important using some definition. While there are many measures of dynamic importance, one of the measures that has been of greatest interest to structural dynamicists, is the contribution of each mode to the dynamic loads at an interface. Dynamically important modes contribute significantly to the interface loads and must be retained in any reduced analytical representation. These modes must be identified during a ground vibration test to validate the corresponding finite element model. Structural dynamicists have used interface load based effective mass measures to efficiently identify target modes for constrained structures. The advantage of these measures of dynamic importance is that they are absolute, in contrast to other measures that only indicate the importance of one mode shape relative to another. However, in many situations, especially in aerospace applications, structures must be tested in a free–free configuration. In the case of free–free elastic modes, the effective mass values are zero, making them useless measures of dynamic importance. This paper presents a new effective mass like measure of absolute dynamic importance that can be applied to free–free structures. The new method is derived based upon the free–free modal equations of motion. The approach is shown to be directly related to ranking mode shapes based on approximate balanced singular values. But, unlike the approximate balanced singular value approach, it is an absolute measure of importance. A numerical example of a general spacecraft system is presented to illustrate the application of the new technique. Dynamically important mode shapes were easily identified for modal acceleration, velocity, and displacement output. The new method provides an efficient technique for selecting target modes for a modal vibration test, or the reduction of a modal based analytical model to the dynamically important mode shapes. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Generalization of Effective Mass for Selecting Free–Free Target Modes | |
| type | Journal Paper | |
| journal volume | 129 | |
| journal issue | 1 | |
| journal title | Journal of Vibration and Acoustics | |
| identifier doi | 10.1115/1.2424980 | |
| journal fristpage | 121 | |
| journal lastpage | 127 | |
| identifier eissn | 1528-8927 | |
| keywords | Electromagnetic fields | |
| keywords | Stress | |
| keywords | Displacement | |
| keywords | Finite element model | |
| keywords | Shapes | |
| keywords | Space vehicles | |
| keywords | Equations of motion | |
| keywords | Enterprise information management | |
| keywords | Vibration tests | |
| keywords | Degrees of freedom AND Aerospace industry | |
| tree | Journal of Vibration and Acoustics:;2007:;volume( 129 ):;issue: 001 | |
| contenttype | Fulltext |