Dynamic Loading on Turbofan Blades Due to Bird-Strike
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[1] Sunil K. Sinha,et al. Dynamic Loads in the Fan Containment Structure of a Turbofan Engine , 2009 .
[2] Wang Fusheng,et al. Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation , 2007 .
[3] R. N. Tadros,et al. Analytical and Experimental Simulation of Fan Blade Behavior and Damage Under Bird Impact , 1991 .
[4] Francesco Marulo,et al. Design and Testing of a Fiber-Metal-Laminate Bird-Strike-Resistant Leading Edge , 2009 .
[5] N. F. Martin,et al. Nonlinear finite-element analysis to predict fan-blade damage due tosoft-body impact , 1990 .
[6] Marco Anghileri,et al. Birdstrike onto the Composite Intake of a Turbofan Engine , 2005 .
[7] Andrew J. Gunnion,et al. Bird-strike simulation for certification of the Boeing 787 composite moveable trailing edge , 2008 .
[8] Ivica Smojver,et al. Numerical simulation of bird strike damage prediction in airplane flap structure , 2010 .
[9] S. Timoshenko,et al. THEORY OF PLATES AND SHELLS , 1959 .
[10] Thomas J. Vasko,et al. Robust Bird-Strike Modeling Based on ALE Formulation Using LS-DYNA , 2006 .
[11] Kunigal N. Shivakumar,et al. Prediction of Impact Force and Duration Due to Low-Velocity Impact on Circular Composite Laminates , 1985 .
[12] Francesco Marulo,et al. Analysis of Bird Impact on a Composite Tailplane Leading Edge , 2008 .
[13] James F. Doyle. Experimentally determining the contact force during the transverse impact of an orthotropic plate , 1987 .
[14] L. Schwer. Impact of a 3D Woven Textile Composite Thin Panel: Damage and Failure Modeling , 1999 .
[15] Alessandro Airoldi,et al. Modelling of impact forces and pressures in Lagrangian bird strike analyses , 2006 .
[16] E. Niering. Simulation of bird strikes on turbine engines , 1990 .
[17] E. Deletombe,et al. Assessment of multi-physics FE methods for bird strike modelling-Application to a metallic riveted airframe , 2002 .
[18] Augustin Gakwaya,et al. Review of existing numerical methods and validation procedure available for bird strike modelling , 2007 .
[19] W. Paepegem,et al. Use of projection moiré for measuring the instantaneous out-of-plane deflections of composite plates subject to bird strike , 2008 .
[20] Robin Olsson,et al. Closed form prediction of peak load and delamination onset under small mass impact , 2003 .
[21] James L. Rand,et al. The Development of a Substitute Bird Model , 1981 .
[22] G. N. Labeas,et al. Bird strike simulation on a novel composite leading edge design , 2006 .
[23] Magnus Langseth,et al. A numerical model for bird strike of aluminium foam-based sandwich panels , 2006 .
[24] Sunil K. Sinha,et al. Combined Torsional-Bending-Axial Dynamics of a Twisted Rotating Cantilever Timoshenko Beam With Contact-Impact Loads at the Free End , 2007 .
[25] E. Fehlberg. New High‐Order Runge‐Kutta Formulas with Step Size Control for Systems of First‐and Second‐Order Differential Equations , 1964 .
[26] Shaker A. Meguid,et al. Transient three dimensional finite element analysis of a bird striking a fan blade , 2008 .
[27] Alastair Johnson,et al. Numerical prediction of damage in composite structures from soft body impacts , 2006 .
[28] M. A. McCarthy,et al. Modelling of Bird Strike on an Aircraft Wing Leading Edge Made from Fibre Metal Laminates – Part 2: Modelling of Impact with SPH Bird Model , 2004 .
[29] E. Fehlberg,et al. New High‐Order Runge‐Kutta Formulas with an Arbitrarily Small Truncation Error , 1966 .
[30] Sunil K. Sinha,et al. Natural frequencies of a pre-twisted blade in a centrifugal force field , 2011 .
[31] Hyonny Kim,et al. Modeling Hail Ice Impacts and Predicting Impact Damage Initiation in Composite Structures , 2000 .
[32] Nik Petrinic,et al. Modelling bird impacts on an aircraft wing – Part 1: Material modelling of the fibre metal laminate leading edge material with continuum damage mechanics , 2005 .