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Flutter is dynamic instability which is caused by the interaction of aerodynamic, inertial, and structural forces. Flutter in aircraft structure, can cause structural failure and limit the aircraft flight domain. Therefore, this phenomenon must be analyzed since the preliminary design to anticipate...
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id-itb.:107582017-10-09T10:33:28Z#TITLE_ALTERNATIVE# MAYANG MAHASTI (NIM 13603007), KATIA Indonesia Final Project INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/10758 Flutter is dynamic instability which is caused by the interaction of aerodynamic, inertial, and structural forces. Flutter in aircraft structure, can cause structural failure and limit the aircraft flight domain. Therefore, this phenomenon must be analyzed since the preliminary design to anticipate structural catastrophic failure. Aircraft part which has the highest risk of flutter is wing and tail (vertical and horizontal). This research analyzed flutter happened on F-16 fighter which carries missile on each wing. Flutter is analyzed in various parameters. The parameters to be analyzed are the number of missiles, the location of missiles, and different Mach numbers. The analysis is carried out to analyzed dynamic and flutter characteristic on F-16 fighter, so the best configuration of missile location can be obtained. The determination of dynamic and flutter characteristic is carried out using MSC Nastran. text |
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Indonesia |
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Flutter is dynamic instability which is caused by the interaction of aerodynamic, inertial, and structural forces. Flutter in aircraft structure, can cause structural failure and limit the aircraft flight domain. Therefore, this phenomenon must be analyzed since the preliminary design to anticipate structural catastrophic failure. Aircraft part which has the highest risk of flutter is wing and tail (vertical and horizontal). This research analyzed flutter happened on F-16 fighter which carries missile on each wing. Flutter is analyzed in various parameters. The parameters to be analyzed are the number of missiles, the location of missiles, and different Mach numbers. The analysis is carried out to analyzed dynamic and flutter characteristic on F-16 fighter, so the best configuration of missile location can be obtained. The determination of dynamic and flutter characteristic is carried out using MSC Nastran. |
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Final Project |
| author |
MAYANG MAHASTI (NIM 13603007), KATIA |
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MAYANG MAHASTI (NIM 13603007), KATIA #TITLE_ALTERNATIVE# |
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MAYANG MAHASTI (NIM 13603007), KATIA |
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MAYANG MAHASTI (NIM 13603007), KATIA |
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https://digilib.itb.ac.id/gdl/view/10758 |
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1820665953412710400 |