Citation: | CHEN K,LIU X Y,CHENG P,et al. Research on the static aero-elastic sensitivity of stiffness of flexible wing[J]. Journal of Experiments in Fluid Mechanics,2022,36(6):54-60.. DOI: 10.11729/syltlx20210013 |
[1] |
TILMANN C P, FLICK P M, MARTIN C A, et al. High altitude long endurance technologies for sensor craft[C]// Proc of Novel Vehicle Concepts and Emerging Vehicle Technologies Symposium. 2003.
|
[2] |
NGUYEN N, TRINH K, REYNOLDS K, et al. Elastically shaped wing optimization and aircraft concept for improved cruise efficiency[C]//Proc of the 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine. 2013. doi: 10.2514/6.2013-141
|
[3] |
NOLL T E, BROWN J M, PEREZ-DAVIS M E, et al. Investigation of the Helios prototype aircraft mishap: volume I mishap report[R]. VA 23681-2199, 2004.
|
[4] |
BHATIA K, WERTHEIMER J. Aeroelastic challenges for a high speed civil transport[C]//Proc of the 34th Structures, Structural Dynamics and Materials Conference. 1993. doi: 10.2514/6.1993-1478
|
[5] |
CORMAN J A, SAROJINI D, GHARBI A, et al. Estimating jig shape for an aircraft wing determined through aerodynamic shape optimization with rigid body assumptions[C]//Proc of the AIAA Scitech 2019 Forum. 2019. doi: 10.2514/6.2019-0418
|
[6] |
WAN Z Q,LIANG L,YANG C. Method of the jig shape design for a flexible wing[J]. Journal of Aircraft,2014,51(1):327-330. doi: 10.2514/1.C031926
|
[7] |
ZINK P S,RAVEH D E,MAVRIS D N. Integrated trim and structural design process for active aeroelastic wing technology[J]. Journal of Aircraft,2003,40(3):523-531. doi: 10.2514/2.3126
|
[8] |
BISPLINGHOF R L, ASHLEY H, HALFMAN T L. Aeroelasticity[M]. New York: John Wiley and Sons, Inc. , 1962.
|
[9] |
SCHUSTER D M. An inverse method for computation of structural stiffness distributions of aeroelastically optimized wings[R]. AIAA-1993-1540, 1993. doi: 10.2514/6.1993-1540
|
[10] |
刘东岳,万志强,杨超,等. 大展弦比机翼总体刚度的气动弹性优化设计[J]. 航空学报,2011,32(6):1025-1031.
LIU D Y,WAN Z Q,YANG C,et al. Aeroelastic optimization design of global stiffness for high aspect ratio wing[J]. Acta Aeronautica et Astronautica Sinica,2011,32(6):1025-1031.
|
[11] |
张建刚,孙仁俊,金鑫. 大展弦比后掠机翼静气弹效应对气动载荷的影响实验与分析[J]. 应用力学学报,2017,34(3):570-575,616.
ZHANG J G,SUN R J,JIN X. Test and study of static aeroelastic effects on wing's aerodynamic load[J]. Chinese Journal of Applied Mechanics,2017,34(3):570-575,616.
|
[12] |
JAMESON A, SCHMIDT W, TURKEL E. Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes[C]//Proc of the 14th Fluid and Plasma Dynamics Conference. 1981. doi: 10.2514/6.1981-1259
|
[13] |
MENTER F R. Two-equation eddy-viscosity turbulence models for engineering applications[J]. AIAA Journal,1994,32(8):1598-1605. doi: 10.2514/3.12149
|
[14] |
HARDER R L,DESMARAIS R N. Interpolation using surface splines[J]. Journal of Aircraft,1972,9(2):189-191. doi: 10.2514/3.44330
|
[15] |
BURG C. A robust unstructured grid movement strategy using three-dimensional torsional springs[C]//Proc of the 34th AIAA Fluid Dynamics Conference and Exhibition. 2004. doi: 10.2514/6.2004-2529
|
[16] |
MAO K, XUE F, BAI F, et al. An engineering correction method of static aeroelasticity and Reynolds number effect on wind tunnel pressure distribution[M]//Singapore: Springer Singapore, 2019: 114-134. doi: 10.1007/978-981-13-3305-7_10
|
[17] |
ADELMAN H M,HAFTKA R T. Sensitivity analysis of discrete systems[J]. Progress in Astronautics and Aeronautics,1993,150:291-291.
|
[18] |
HAFTKA R T,ADELMAN H M. Recent developments in structural sensitivity analysis[J]. Structural Optimization,1989,1(3):137-151. doi: 10.1007/BF01637334
|
[19] |
万志强,杨超. 设计敏度在气动弹性遗传优化中的应用[J]. 北京航空航天大学学报,2006,32(5):508-512. DOI: 10.3969/j.issn.1001-5965.2006.05.003
WAN Z Q,YANG C. Application of design sensitivity in aeroelastic genetic optimization[J]. Journal of Beijing University of Aeronautics and Astronautics,2006,32(5):508-512. doi: 10.3969/j.issn.1001-5965.2006.05.003
|