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유한요소 해석을 이용한 Missile Guidance Structure의 Random response analysisRandom response analysis of Missile Guidance Structure by using Finite Element Method
- Other Titles
- Random response analysis of Missile Guidance Structure by using Finite Element Method
- Issue Date
- 2015
- Publisher
- 항공우주시스템공학회
- Keywords
- Random Response; Finite Element Method; Missile Guidance; Frequency Analysis; Mil-STD-810G; Mode shape; Acceleration Spectrum Density
- Citation
- 항공우주시스템공학회지, v.9, no.2, pp 51 - 56
- Pages
- 6
- Journal Title
- 항공우주시스템공학회지
- Volume
- 9
- Number
- 2
- Start Page
- 51
- End Page
- 56
- Abstract
- In the vibration test, Most of the test specifications is standardized methods of sinusoidal excitation. However, in accordance with the ability of the test equipment progress and developments of electronic technology, methods of random vibration test is standardized in the MIL standard. Therefore, in this study, we tried to analyze Missile Guidance Structure using a finite element analysis with ABAQUS 6.13 that is commercial program. First, Random response analysis is analyzed. Following analyzing the results, we wanted to find the model that is lightweight and resonance does not occur.
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Collections - 공학계열 > 기계항공우주공학부 > Journal Articles
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