| Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring B Stanford, P Ifju, R Albertani, W Shyy Progress in Aerospace Sciences 44 (4), 258-294, 2008 | 216 | 2008 |
| Computational aerodynamics of low Reynolds number plunging, pitching and flexible wings for MAV applications W Shyy, Y Lian, J Tang, H Liu, P Trizila, B Stanford, L Bernal, C Cesnik, ... Acta Mechanica Sinica 24, 351-373, 2008 | 210 | 2008 |
| Aerodynamic coefficients and deformation measurements on flexible micro air vehicle wings R Albertani, B Stanford, JP Hubner, PG Ifju Experimental Mechanics 47, 625-635, 2007 | 171 | 2007 |
| Analytical sensitivity analysis of an unsteady vortex-lattice method for flapping-wing optimization BK Stanford, PS Beran Journal of Aircraft 47 (2), 647-662, 2010 | 153 | 2010 |
| Optimal topology of aircraft rib and spar structures under aeroelastic loads BK Stanford, PD Dunning Journal of Aircraft 52 (4), 1298-1311, 2015 | 125 | 2015 |
| Flapping wing structural deformation and thrust correlation study with flexible membrane wings P Wu, P Ifju, B Stanford AIAA journal 48 (9), 2111-2122, 2010 | 108 | 2010 |
| Global optimization of actively morphing flapping wings M Ghommem, MR Hajj, DT Mook, BK Stanford, PS Beran, RD Snyder, ... Journal of Fluids and Structures 33, 210-228, 2012 | 93 | 2012 |
| Aeroelastic topology optimization of membrane structures for micro air vehicles B Stanford, P Ifju Structural and Multidisciplinary Optimization 38, 301-316, 2009 | 89 | 2009 |
| Uncertainty quantification in aeroelasticity P Beran, B Stanford, C Schrock Annual review of fluid mechanics 49 (1), 361-386, 2017 | 88 | 2017 |
| Static aeroelastic model validation of membrane micro air vehicle wings B Stanford, M Sytsma, R Albertani, D Viieru, W Shyy, P Ifju AIAA journal 45 (12), 2828-2837, 2007 | 85 | 2007 |
| Aeroelastic benefits of tow steering for composite plates BK Stanford, CV Jutte, KC Wu Composite Structures 118, 416-422, 2014 | 81 | 2014 |
| Investigation of membrane actuation for roll control of a micro air vehicle B Stanford, M Abdulrahim, R Lind, P Ifju Journal of Aircraft 44 (3), 741-749, 2007 | 81 | 2007 |
| Structural dynamics and aerodynamics measurements of biologically inspired flexible flapping wings P Wu, BK Stanford, E Sällström, L Ukeiley, PG Ifju Bioinspiration & biomimetics 6 (1), 016009, 2011 | 79 | 2011 |
| Comparison of curvilinear stiffeners and tow steered composites for aeroelastic tailoring of aircraft wings BK Stanford, CV Jutte Computers & Structures 183, 48-60, 2017 | 73 | 2017 |
| Coupled aerostructural topology optimization using a level set method for 3D aircraft wings PD Dunning, BK Stanford, HA Kim Structural and Multidisciplinary Optimization 51, 1113-1132, 2015 | 70 | 2015 |
| Aeroelastic topology optimization of blade-stiffened panels B Stanford, P Beran, M Bhatia Journal of Aircraft 51 (3), 938-944, 2014 | 66 | 2014 |
| Aeroelastic tailoring of transport aircraft wings: state-of-the-art and potential enabling technologies C Jutte, BK Stanford | 66 | 2014 |
| Direct flutter and limit cycle computations of highly flexible wings for efficient analysis and optimization B Stanford, P Beran Journal of Fluids and Structures 36, 111-123, 2013 | 62 | 2013 |
| A computational and experimental studies of flexible wing aerodynamics H Aono, SK Chimakurthi, P Wu, E Sallstrom, B Stanford, C Cesnik, P Ifju, ... 48th AIAA aerospace sciences meeting including the new horizons forum and …, 2010 | 61 | 2010 |
| Aeroelastic tailoring of the NASA common research model via novel material and structural configurations CV Jutte, B Stanford, CD Wieseman, JB Moore 52nd aerospace sciences meeting, 0598, 2014 | 56 | 2014 |
Philip BeranPrincipal Research Aerospace Engineer, Air Force Research Laboratory在 us.af.mil 的电子邮件经过验证
