| Year |
Citation |
Score |
| 2020 |
Hang X, Su W, Fei Q, Jiang D. Analytical sensitivity analysis of flexible aircraft with the unsteady vortex-lattice aerodynamic theory Aerospace Science and Technology. 99: 105612. DOI: 10.1016/J.Ast.2019.105612 |
0.401 |
|
| 2019 |
Su W, Song W. A real-time hybrid aeroelastic simulation platform for flexible wings Aerospace Science and Technology. 95: 105513. DOI: 10.1016/J.Ast.2019.105513 |
0.372 |
|
| 2019 |
Tsushima N, Yokozeki T, Su W, Arizono H. Geometrically nonlinear static aeroelastic analysis of composite morphing wing with corrugated structures Aerospace Science and Technology. 88: 244-257. DOI: 10.1016/J.Ast.2019.03.025 |
0.453 |
|
| 2019 |
He T, Zhu GG, Swei SS-, Su W. Smooth-switching LPV control for vibration suppression of a flexible airplane wing Aerospace Science and Technology. 84: 895-903. DOI: 10.1016/J.Ast.2018.11.029 |
0.365 |
|
| 2018 |
He T, Al-Jiboory AK, Zhu GG, Swei SS-, Su W. Application of ICC LPV control to a blended-wing-body airplane with guaranteed H∞ performance Aerospace Science and Technology. 81: 88-98. DOI: 10.1016/J.Ast.2018.07.046 |
0.314 |
|
| 2018 |
Tsushima N, Su W. A study on adaptive vibration control and energy conversion of highly flexible multifunctional wings Aerospace Science and Technology. 79: 297-309. DOI: 10.1016/J.Ast.2018.05.056 |
0.334 |
|
| 2018 |
Hammerton JR, Su W, Zhu G, Swei SS. Optimum distributed wing shaping and control loads for highly flexible aircraft Aerospace Science and Technology. 79: 255-265. DOI: 10.1016/J.Ast.2018.05.045 |
0.386 |
|
| 2017 |
Al-Jiboory AK, Zhu G, Swei SS, Su W, Nguyen NT. LPV Modeling of a Flexible Wing Aircraft Using Modal Alignment and Adaptive Gridding Methods. Aerospace Science and Technology. 66: 92-102. PMID 29217966 DOI: 10.1016/J.Ast.2017.03.009 |
0.329 |
|
| 2017 |
Su W. Development of an Aeroelastic Formulation for Deformable Airfoils Using Orthogonal Polynomials Aiaa Journal. 55: 2793-2807. DOI: 10.2514/1.J055665 |
0.351 |
|
| 2017 |
Tsushima N, Su W. Concurrent Active Piezoelectric Control and Energy Harvesting of Highly Flexible Multifunctional Wings Journal of Aircraft. 54: 724-736. DOI: 10.2514/1.C033846 |
0.446 |
|
| 2017 |
Su W, King CK, Clark SR, Griffin ED, Suhey JD, Wolf MG. Dynamic Beam Solutions for Real-Time Simulation and Control Development of Flexible Rockets Journal of Spacecraft and Rockets. 54: 403-416. DOI: 10.2514/1.A33543 |
0.355 |
|
| 2017 |
Tsushima N, Su W, Gutierrez H, Wolf MG, Griffin ED, Whittaker JT, Dumoulin MP. Monitoring multi-axial vibrations of flexible rockets using sensor-instrumented reference strain structures Aerospace Science and Technology. 71: 285-298. DOI: 10.1016/J.Ast.2017.09.026 |
0.332 |
|
| 2017 |
Tsushima N, Su W. Flutter suppression for highly flexible wings using passive and active piezoelectric effects Aerospace Science and Technology. 65: 78-89. DOI: 10.1016/J.Ast.2017.02.013 |
0.421 |
|
| 2016 |
Su W, Swei SS, Zhu GG. Optimum Wing Shape Determination of Highly Flexible Morphing Aircraft for Improved Flight Performance. Journal of Aircraft. 53: 1305-1316. PMID 29348697 DOI: 10.2514/1.C033490 |
0.47 |
|
| 2016 |
Tsushima N, Su W. Modeling of Highly Flexible Multifunctional Wings for Energy Harvesting Journal of Aircraft. 53: 1033-1044. DOI: 10.2514/1.C033496 |
0.438 |
|
| 2016 |
Butler NS, Su W, Magar KST, Reich GW. Estimation of morphing airfoil shape and aerodynamic load using artificial hair sensors Proceedings of Spie. 9803: 980329. DOI: 10.1117/12.2219520 |
0.372 |
|
| 2016 |
Su W, Reich GW. Artificial hair sensor designs for flow measurement of UAVs with different scales Proceedings of Spie. 9803. DOI: 10.1117/12.2219188 |
0.32 |
|
| 2015 |
Su W, Reich GW. Gust alleviation of highly flexible UAVs with artificial hair sensors Proceedings of Spie. 9435. DOI: 10.1117/12.2085575 |
0.473 |
|
| 2015 |
Song W, Su W. A wind turbine hybrid simulation framework considering aeroelastic effects Proceedings of Spie. 9435. DOI: 10.1117/12.2084431 |
0.331 |
|
| 2014 |
Su W, Cesnik CES. Strain-Based Analysis for Geometrically Nonlinear Beams: A Modal Approach Journal of Aircraft. 51: 890-903. DOI: 10.2514/1.C032477 |
0.46 |
|
| 2012 |
Cesnik CES, Senatore PJ, Su W, Atkins EM, Shearer CM. X-HALE: A very flexible unmanned aerial vehicle for nonlinear aeroelastic tests Aiaa Journal. 50: 2820-2833. DOI: 10.2514/1.J051392 |
0.528 |
|
| 2011 |
Su W, Cesnik CES. Dynamic Response of Highly Flexible Flying Wings Aiaa Journal. 49: 324-339. DOI: 10.2514/1.J050496 |
0.51 |
|
| 2011 |
Su W, Cesnik CES. Strain-based geometrically nonlinear beam formulation for modeling very flexible aircraft International Journal of Solids and Structures. 48: 2349-2360. DOI: 10.1016/J.Ijsolstr.2011.04.012 |
0.386 |
|
| 2010 |
Su W, Cesnik CES. Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft Journal of Aircraft. 47: 1539-1553. DOI: 10.2514/1.47317 |
0.501 |
|
| Show low-probability matches. |