Bret Stanford

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Philip BeranPrincipal Research Aerospace Engineer, Air Force Research LaboratoryEmail verificata su us.af.mil
Pin WuEmail verificata su ufl.edu
Carlos E. S. CesnikClarence L. "Kelly" Johnson Professor of Aerospace Engineering, The University of MichiganEmail verificata su umich.edu
James HubnerProfessor, University of AlabamaEmail verificata su eng.ua.edu
Hyunsun Alicia KimUC San DiegoEmail verificata su ucsd.edu
Peter DunningLecturer, University of AberdeenEmail verificata su abdn.ac.uk
Mohammad H. KurdiFord Motor CompanyEmail verificata su ford.com
Lawrence UkeileyUniversity of FloridaEmail verificata su ufl.edu
Satish Kumar Chimakurthi, Ph.D.President and CEO of Epitome Research and Innovations Inc.Email verificata su epitomeri.com
Vijay JagdaleSenior Engineer / Research Scientist, United Technologies Research Center, East Hartford, CTEmail verificata su utrc.utc.com
Manav BhatiaMississippi State UniversityEmail verificata su msstate.edu
Mayuresh PatilGeorgia TechEmail verificata su gatech.edu
Yongsheng LianUniversity of LouisvilleEmail verificata su louisville.edu
Pat TrizilaEmail verificata su umich.edu
Liu HaoMoffitt Cancer CenterEmail verificata su moffitt.org
Mujahid AbdulrahimUniversity of Missouri Kansas CityEmail verificata su umkc.edu
Craig WoolseyAerospace & Ocean Engineering, Virginia TechEmail verificata su vt.edu
Hikaru AonoDepartment of Mechanical Engineering and Robotics, Shinshu UniversityEmail verificata su shinshu-u.ac.jp
BV SankarUniversity of FloridaEmail verificata su ufl.edu
Paul M WeaverBernal Chair in Composite Structures, Uni Limerick; Prof. in Lightweight Structures, Uni Bristol;Email verificata su ul.ie

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Bret Stanford

NASA Langley Research Center

Email verificata su nasa.gov


Titolo Ordina per citazioni Ordina per anno Ordina per titolo	Citata da Citata da	Anno
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

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