Metamodels for Composite Lattice Fuselage Design [PDF]
International Journal of Materials, Mechanics and Manufacturing, 2015 Liu, Dianzi, Zhou, Xue, Toropov, Vassili
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Structural Vibration Analysis of UAVs Under Ground Engine Test Conditions. [PDF]
Sensors (Basel)González-Cabrera SI +5 more
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Insect-scale flapping-wing MAVs with variable transmission ratio and wingspan: achieving payload adaptability, and self-stabilizing hovering. [PDF]
Microsyst NanoengLu X +5 more
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Composite fuselage technology [PDF]
The overall objective is to identify and understand, via directed experimentation and analysis, the mechanisms which control the structural behavior of fuselages in their response to damage (resistance, tolerance, and arrest).
Graves, Michael J., Lagace, Paul A.
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Natural frequency and modal analysis of tractor vibration system. [PDF]
Sci RepYuan JQ, Zhang L.
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Cost-Effectiveness of Structural Health Monitoring in Aviation: A Literature Review. [PDF]
Sensors (Basel)Ballarin P, Sala G, Airoldi A.
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Design of Glider Airborne Wind Turbine. [PDF]
ScientificWorldJournalAkour SN +4 more
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Harmonic adaptive fault-tolerant control for incipient and multiple faults of high mobility fighter. [PDF]
Sci RepHu K, Wang Z, Wang J.
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A Deep Learning On-Board Health Monitoring Method for Landing Gear Shock-Absorbing Systems. [PDF]
Sensors (Basel)Li C, Chen W, Qin W.
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Coupled Wing-Fuselage Vibrations.
Coupled Wing-Fuselage Vibrations.胴體の構造が主翼のそれに比して大して剛くない場合には,それ等の間の聯成振動を考へて置く事が必要になる.我々はその目的に向つて種々簡單な場合を研究して來たが,この論文では翼と胴體とがともに斷面も質量分布も均一でないとし,且つ機關部に於ける集中質量をも考慮に入れてその聯成振動を論じたのである.勿論,強制振動を取り自由振動は強制振動の共振の場合から推定した.始めに數理的理論を作り,實際の状態に相當するやうな場合について數値計算を試みた.次に全然同じ状態を表す模型を作り,數値計算の結果と比較し,理論と實驗との一致性を確めたのである.研究の結果によると,聯成振動の場合といへども實際には問題を比較的に簡單に取扱ひ得ることがわかる.主翼が對稱的振動をなす場合には主翼の中央を固定端とし翼端を自由端とする屈曲振動と ...
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