Postcritical Analysis of PrandtlPlane Joined-Wing Configurations
暂无分享,去创建一个
[1] Gian Luca Ghiringhelli,et al. The Lifting System of a PrandtlPlane, Part 1: Design and Analysis of a Light Alloy Structural Solution , 2012 .
[2] Cv Clemens Verhoosel,et al. Non-Linear Finite Element Analysis of Solids and Structures , 1991 .
[3] Luciano Demasi,et al. The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations , 2007 .
[4] Robert A. Canfield,et al. Joined-Wing Aeroelastic Design with Geometric Nonlinearity , 2005 .
[5] Luciano Demasi,et al. Exploratory Studies of Joined Wing Aeroelasticity , 2005 .
[6] Donald L. Kunz,et al. Experiments with Geometric Non-Linear Coupling for Analytical Validation , 2010 .
[7] Mayuresh J. Patil. NONLINEAR AEROELASTIC ANALYSIS OF JOINED-WING AIRCRAFT , 2003 .
[8] Terrence A. Weisshaar,et al. Aeroelasticity of Nonconventional Airplane Configurations-Past and Future , 2003 .
[9] Weihua Su,et al. Coupled nonlinear aeroelasticity and flight dynamics of fully flexible aircraft , 2008 .
[10] A. Frediani,et al. Best wing system: an exact solution of the Prandtl’s problem , 2009 .
[11] Luciano Demasi,et al. Nonlinear Analysis of PrandtlPlane Joined Wings - Part II: Effects of Anisotropy , 2012 .
[12] Aldo Frediani,et al. The PrandtlPlane Configuration: Overview on Possible Applications to Civil Aviation , 2012 .
[13] Aldo Frediani. Velivolo Biplano ad ali contrapposte , 2003 .
[14] Aldo Frediani. New Large Aircraft , 1999 .
[15] E. Riks. The Application of Newton's Method to the Problem of Elastic Stability , 1972 .
[16] Ekkehard Ramm,et al. Strategies for Tracing the Nonlinear Response Near Limit Points , 1981 .
[17] E. Riks. An incremental approach to the solution of snapping and buckling problems , 1979 .
[18] J. Wolkovitch,et al. The joined wing - An overview , 1985 .
[19] Dewey H. Hodges,et al. Incremental Method for Structural Analysis of Joined-Wing Aircraft , 2011 .
[20] Aldo Frediani,et al. Application of Optimisation Algorithms to Aircraft Aerodynamics , 2009 .
[21] P. Wriggers. Nonlinear Finite Element Methods , 2008 .
[22] Dewey H. Hodges,et al. Parametric Study of Joined-Wing Aircraft Geometry , 2010 .
[23] William R. Spillers,et al. Analysis of Geometrically Nonlinear Structures , 1994 .
[24] Raphael T. Haftka,et al. Multidisciplinary Design Optimization of a Transonic Commercial Transport with Strut-Braced Wing , 2001 .
[25] Robert A. Canfield,et al. Structural Optimization of Joined-Wing Beam Model with Bend/Twist Coupling Using ESL , 2009 .
[26] Raymond M. Kolonay,et al. Nonlinear Response Structural Optimization of a Joined Wing Using Equivalent Loads , 2008 .
[27] Michel van Tooren,et al. Automated Control Surface Design and Sizing for the Prandtl Plane , 2010 .
[28] M. Crisfield. A FAST INCREMENTAL/ITERATIVE SOLUTION PROCEDURE THAT HANDLES "SNAP-THROUGH" , 1981 .
[29] Dimitri N. Mavris,et al. Design Optimization of a Truss-Braced-Wing Transonic Transport Aircraft , 2010 .
[30] L. Demasi. Induced Drag Minimization: A Variational Approach Using the Acceleration Potential , 2006 .
[31] Robert Levy,et al. The geometric stiffness of triangular composite-materials shell elements , 2005 .
[32] Aldo Frediani,et al. The Lifting System of a PrandtlPlane, Part 2: Preliminary Study on Flutter Characteristics , 2012 .