| The UTwente aeroacoustic wind tunnel upgrade LD de Santana, MP Sanders, CH Venner, HW Hoeijmakers 2018 AIAA/CEAS Aeroacoustics Conference, 3136, 2018 | 50 | 2018 |
| Unsteady Surface Pressure Measurements on Trailing Edge Serrations Based on Digital MEMS Microphones. MP Sanders, LD De Santana, M Azarpeyvand, CH Venner 2018 AIAA/CEAS Aeroacoustics Conference, 3290, 2018 | 19 | 2018 |
| Trailing-edge noise comparability in open, closed, and hybrid wind tunnel test sections MPJ Sanders, CFJ Koenjer, L Botero-Bolivar, FL dos Santos, CH Venner, ... AIAA journal 60 (7), 4053-4067, 2022 | 18 | 2022 |
| Influence of tripping devices in hastening transition in a flat plate submitted to zero and favorable pressure gradients FL Dos Santos, MP Sanders, L Dantas de Santana, C H. Venner AIAA Scitech 2020 Forum, 0046, 2020 | 12 | 2020 |
| Comparison between analog and digital phased microphone arrays for aeroacoustic measurements R Merino-Martinez, MP Sanders, L Caldas, F Avallone, D Ragni, ... 2018 AIAA/CEAS Aeroacoustics Conference, 2809, 2018 | 12 | 2018 |
| A forced‐choice preferential looking task for the assessment of vision in dogs: pilot study KL Graham, SE Byosiere, LC Feng, M Sanders, PC Bennett, K Caruso, ... Journal of Small Animal Practice 60 (6), 340-347, 2019 | 9 | 2019 |
| The Boundary layer over a flat plate MPJ Sanders University of Twente, 2014 | 8 | 2014 |
| Experimental characterization of vortex generators induced noise of wind turbines D Kolkman, LD de Santana, CH Venner, A Garrel, C Arce León, ... 2018 AIAA/CEAS Aeroacoustics Conference, 2800, 2018 | 6 | 2018 |
| Slat noise measurements in open-jet, hard-wall and hybrid wind tunnel test sections MPJ Sanders, CH Venner, LD de Santana Journal of Sound and Vibration 546, 117420, 2023 | 5 | 2023 |
| The Sweep Angle Effect on Slat Noise Characteristics of the 30P30N High-Lift Model in an Open-Jet Wind Tunnel. MP Sanders, LD de Santana, CH Venner AIAA Aviation 2020 Forum, 2557, 2020 | 5 | 2020 |
| Airfoil Trailing-Edge Noise in an Open-Jet, a Hard-Wall and a Hybrid Test Section Wind Tunnel: A Benchmark Exercise MP Sanders, C Koenjer, LB Bolivar, FL Dos Santos, CH Venner, ... AIAA Aviation Forum 2021, 2021 | 4 | 2021 |
| Airfoil Trailing Edge Noise Measurements in an Open-jet, Hard-wall and Kevlar-wall Test Section: a Benchmark Exercise. MP Sanders, L Botero, LD de Santana, C Venner AIAA AVIATION 2021 FORUM, 2253, 2021 | 3 | 2021 |
| Aeroacoustic measurements of airframe components: in an open-jet, a hard-wall and a hybrid wind tunnel test section MP Sanders | 2 | 2022 |
| Comparability of High-Lift Noise Measurements in a Kevlar-Wall, a Hard-Wall and an Open-Jet Test Section. MP Sanders, LD de Santana, C Venner AIAA AVIATION 2021 FORUM, 2252, 2021 | 1 | 2021 |
| An analysis of slat noise using prediction models L Botero-Bolivar, M Sanders, L De Santana, F Catalano Forum Acusticum, 1507-1514, 2020 | 1 | 2020 |
| Analysis of a semi-empirical leading-edge slat noise prediction model LB Bolivar, MPJ Sanders, LD De Santana, CH Venner, FM Catalano Forum Acousticum, E-FA 2020, 2020 | 1 | 2020 |
| Investigation of Leading-Edge Vortex Formation on a Robotic Bird’s Wing. L Schalk University of Twente, 2022 | | 2022 |
| Erratum to: Search for new phenomena in final states with an energetic jet and large missing transverse momentum in pp collisions at\documentclass [12pt]{minimal}\usepackage … G Aad, B Abbott, J Abdallah, S Abdel Khalek, R Aben, B Abi, M Abolins, ... Springer Berlin Heidelberg, 2015 | | 2015 |
| Measurement of three-jet production cross-sections in\documentclass [12pt]{minimal}\usepackage {amsmath}\usepackage {wasysym}\usepackage {amsfonts}\usepackage {amssymb … G Aad, B Abbott, J Abdallah, S Abdel Khalek, R Aben, B Abi, M Abolins, ... Springer Berlin Heidelberg, 2015 | | 2015 |
| Jet energy measurement and its systematic uncertainty in proton–proton collisions at\documentclass [12pt]{minimal}\usepackage {amsmath}\usepackage {wasysym}\usepackage … G Aad, T Abajyan, B Abbott, J Abdallah, S Abdel Khalek, R Aben, B Abi, ... Springer Berlin Heidelberg, 2015 | | 2015 |
