Investigations of passive wing technologies for load reduction
暂无分享,去创建一个
W. R. Krüger | J. Dillinger | R. De Breuker | K. Haydn | W. Krüger | R. De Breuker | J. Dillinger | K. Haydn
[1] J. Cooper,et al. Testing of Folding Wing-Tip for Gust Load Alleviation in High Aspect Ratio Wing , 2019, AIAA Scitech 2019 Forum.
[2] Thomas Klimmek,et al. Loads and Structural Optimization Process for Composite Long Range Transport Aircraft Configuration , 2018, 2018 Multidisciplinary Analysis and Optimization Conference.
[3] Roeland De Breuker,et al. Adaptive wing: Investigations of passive wing technologies for loads reduction in the cleansky smart fixed wing aircraft (SFWA) project , 2016 .
[4] Thomas Klimmek,et al. Static Aeroelastic Stiffness Optimization and Investigation of Forward Swept Composite Wings , 2013 .
[5] Zafer Gürdal,et al. Stiffness Optimization of Composite Wings with Aeroelastic Constraints , 2013 .
[6] Thomas Klimmek,et al. Parameterization of topology and geometry for the multidisciplinary optimization of wing structures , 2009 .
[7] J. Dillinger. Static Aeroelastic Optimization of Composite Wings with Variable Stiffness Laminates , 2014 .
[8] Eli Livne,et al. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs , 2017 .
[9] T. A. Weisshaar,et al. Aeroelastic tailoring - Theory, practice, and promise , 1984 .
[10] T. A. Weisshaar,et al. Optimum design of composite structures , 1989 .
[11] Masaki Kameyama,et al. Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters , 2007 .
[12] Thomas Klimmek,et al. Static aeroelastic stiffness optimization of a forward swept composite wing with CFD-corrected aero loads , 2019, CEAS Aeronautical Journal.
[13] Daniel M. De Leon,et al. Aeroelastic tailoring using fiber orientation and topology optimization , 2012 .
[14] Robert C. Scott,et al. Aeroservoelastic Wind-Tunnel Test of the SUGAR Truss Braced Wing Wind-Tunnel Model , 2015 .
[15] V. B. Venkayya,et al. Design interfaces and data transfer issues in multidisciplinary design , 1996 .
[16] Vassili Toropov,et al. A lamination parameter-based strategy for solving an integer-continuous problem arising in composite optimization , 2013 .
[17] Raphael T. Haftka,et al. Preliminary design of composite wings for buckling, strength and displacement constraints , 1979 .
[18] Ralf Heinrich,et al. The DLR TAU-Code: Recent Applications in Research and Industry , 2006 .
[19] Mostafa M. Abdalla,et al. Blended Composite Optimization combining Stacking Sequence Tables and a Modified Shepard’s Method , 2015 .
[20] Hans-Dieter Joos,et al. Gust load alleviation for a long-range aircraft with and without anticipation , 2019, CEAS Aeronautical Journal.
[21] Thomas Klimmek,et al. Parametric Set-Up of a Structural Model for FERMAT Configuration for Aeroelastic and Loads Analysis , 2014 .
[22] J. Dugundji,et al. Aeroelastic flutter and divergence of stiffness coupled, graphite/epoxy cantilevered plates , 1984 .
[23] Edmund Pendleton,et al. Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development , 2000 .
[24] Christopher D. Regan,et al. Survey of Applications of Active Control Technology for Gust Alleviation and New Challenges for Lighter-Weight Aircraft , 2013 .
[25] Sunpeth Cumnuantip,et al. Design and aeroelastic assessment of a forward-swept wing aircraft , 2014 .
[26] C. Ilic,et al. DLR project Digital-X: towards virtual aircraft design and flight testing based on high-fidelity methods , 2015, CEAS Aeronautical Journal.
[27] Roeland De Breuker,et al. An Aeroelastic Multi-Fidelity Approach for Aeroelastic Tailoring , 2013 .