Optimization of a morphing wing based on coupled aerodynamic and structural constraints P Gamboa, J Vale, FJ P. Lau, A Suleman AIAA journal 47 (9), 2087-2104, 2009 | 111 | 2009 |
A review on non-linear aeroelasticity of high aspect-ratio wings F Afonso, J Vale, E Oliveira, F Lau, A Suleman Progress in Aerospace Sciences 89, 40-57, 2017 | 41 | 2017 |
Design and testing of a morphing wing for an experimental UAV P Gamboa, P Aleixo, J Vale, F Lau, A Suleman UNIVERSITY OF BEIRA INTERIOR COVILHA (PORTUGAL), 2007 | 36 | 2007 |
Aero-structural optimization and performance evaluation of a morphing wing with variable span and camber J Vale, A Leite, F Lau, A Suleman Journal of Intelligent Material Systems and Structures 22 (10), 1057-1073, 2011 | 32 | 2011 |
Prediction of flow-induced noise in transport vehicles: development and validation of a coupled structural-acoustic analytical framework J Da Rocha, A Suleman, F Lau Canadian Acoustics 37 (4), 13-29, 2009 | 21 | 2009 |
Performance based multidisciplinary design optimization of morphing aircraft F Afonso, J Vale, F Lau, A Suleman Aerospace Science and Technology 67, 1-12, 2017 | 19 | 2017 |
On sound generation by moving surfaces and convected sources in a flow L Campos, FJP Lau International Journal of Aeroacoustics 11 (1), 103-135, 2012 | 14 | 2012 |
Flow-induced noise and vibration in aircraft cylindrical cabins: closed-form analytical model validation J da Rocha, A Suleman, F Lau Journal of Vibration and Acoustics 133 (5), 051013, 2011 | 14 | 2011 |
On sound in an inverse sinusoidal nozzle with low Mach number mean flow LMBC Campos, FJP Lau The Journal of the Acoustical Society of America 100 (1), 355-363, 1996 | 14 | 1996 |
Multidisciplinary design optimization of a morphing wing for an experimental UAV J Vale, F Lau, A Suleman, P Gamboa 11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 7131, 2006 | 13 | 2006 |
On the acoustics of low Mach number bulged, throated and baffled nozzles L Campos, FJP Lau Journal of sound and vibration 196 (5), 611-633, 1996 | 12 | 1996 |
On the effect of wall undulations on the acoustics of ducts with flow FJP Lau, L Campos Journal of sound and vibration 270 (1-2), 361-378, 2004 | 11 | 2004 |
Multidisciplinary performance based optimization of morphing aircraft A Suleman, F Lau, J Vale, F Afonso 22nd AIAA/ASME/AHS Adaptive Structures Conference, 0761, 2014 | 10 | 2014 |
Prediction of turbulent boundary layer induced noise in the cabin of a BWB aircraft J Rocha, A Suleman, F Lau Shock and Vibration 19 (4), 693-705, 2012 | 10 | 2012 |
Turbulent boundary layer induced noise and vibration of a multi-panel walled acoustic enclosure J Da Rocha, A Suleman, F Lau Canadian Acoustics 38 (4), 9-22, 2010 | 9 | 2010 |
Smorph-smart aircraft morphing technologies project J Cooper, A Suleman, S Ricci, S Miller, G Vio, G Vio, L da Luz, A Gomes, ... 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2010 | 9 | 2010 |
On the convection of sound in inverse catenoidal nozzles L Campos, FJP Lau Journal of sound and vibration 244 (2), 195-209, 2001 | 8 | 2001 |
Nonlinear aeroelastic scaling of high aspect-ratio wings C Spada, F Afonso, F Lau, A Suleman Aerospace Science and Technology 63, 363-371, 2017 | 7 | 2017 |
Non-linear aeroelastic analysis in the time domain of high-aspect-ratio wings: Effect of chord and taper-ratio variation A Suleman, F Afonso, J Vale, É Oliveira, F Lau The Aeronautical Journal 121 (1235), 21-53, 2017 | 6 | 2017 |
Design and development of strategies and structures for wing morphing J Vale, A Leite, F Lau, A Suleman The Applied Vehicle Technology Panel Symposium (AVT-168), Évora, Portugal, 20-23, 2009 | 6 | 2009 |