Transient analysis of flexible multi-body systems. II. Application to aircraft landing

DOI10.1016/0045-7825(86)90037-XzbMath0575.73067OpenAlexW2059015691MaRDI QIDQ1064150

Yehia A. Khulief, Koorosh Changizi, Ahmed A. Shabana

Publication date: 1986

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(86)90037-x

zbMATH Keywords

Lagrangian formulationtransient analysisdynamic behaviorcheck on constraint violationscomputer- generatedexplicit-implicit direct numerical integration algorithmfinite set of coupled reference and modal coordinatesgeneralized momentum balancegeneralized velocitiesImpactintegrated forward in timeinterconnected rigid and flexible bodiesintermittent motionjoints between different componentslarge angular rotationslarge-scale aircraftlarge-scale multi-body aircraftNewton-Raphson type iterationnonlinear algebraic constraint equationspredict jump discontinuitiessimulate the impact between the landing gear and the runwaysystem equations of motionsystem reaction forces

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30)

Related Items (1)

Transient analysis of flexible multi-body systems. I. Dynamics of flexible bodies

Cites Work

• Transient analysis of flexible multi-body systems. I. Dynamics of flexible bodies
• Substructure synthesis methods for dynamic analysis of multi-body systems
• Impact responses of multi-body systems with consistent and lumped masses

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