In this work, the changes in eigenfrequencies of flexible appendages with • :various mass ratios of space vehicles due to the allowance of a rigid body. motion are studied. These changes are governed by the difference eigen-value problem [2] which is formulated in terms of the generated effective :mass and stiffness matrices. The computation techniques for calculating . • the upper and lower bounds of the dominant eigenfrequencies are performed : by the utilization of the bound formula approach [1] . An example of the transverse vibration analysis of the fuslage-wing combination with diff- erent mass ratios in different zones of vibratory motion is solved . A : 'comparison between the computed calculations and previously published re-sults [0] is presented
MAHER, A., & SCHLACK, A. (1984). QUALITATIVE BEHAVIOR OF EIGENFREQUENCIES FOR FREE VIBRATION OF AEROSPACE VEHICLE APPENDAGES. The International Conference on Applied Mechanics and Mechanical Engineering, 1(1st Conference on Applied Mechanical Engineering.), 1-10. doi: 10.21608/amme.1984.48575
MLA
A. MAHER; A. L. SCHLACK. "QUALITATIVE BEHAVIOR OF EIGENFREQUENCIES FOR FREE VIBRATION OF AEROSPACE VEHICLE APPENDAGES". The International Conference on Applied Mechanics and Mechanical Engineering, 1, 1st Conference on Applied Mechanical Engineering., 1984, 1-10. doi: 10.21608/amme.1984.48575
HARVARD
MAHER, A., SCHLACK, A. (1984). 'QUALITATIVE BEHAVIOR OF EIGENFREQUENCIES FOR FREE VIBRATION OF AEROSPACE VEHICLE APPENDAGES', The International Conference on Applied Mechanics and Mechanical Engineering, 1(1st Conference on Applied Mechanical Engineering.), pp. 1-10. doi: 10.21608/amme.1984.48575
VANCOUVER
MAHER, A., SCHLACK, A. QUALITATIVE BEHAVIOR OF EIGENFREQUENCIES FOR FREE VIBRATION OF AEROSPACE VEHICLE APPENDAGES. The International Conference on Applied Mechanics and Mechanical Engineering, 1984; 1(1st Conference on Applied Mechanical Engineering.): 1-10. doi: 10.21608/amme.1984.48575
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