A parallel, high-order discontinuous Galerkin code for laminar and turbulent flows B Landmann, M Kessler, S Wagner, E Krämer Computers & Fluids 37 (4), 427-438, 2008 | 105 | 2008 |
Source-time dominant aeroacoustics M Kessler, S Wagner Computers & fluids 33 (5-6), 791-800, 2004 | 70 | 2004 |
Electrical powered tail rotor of a helicopter A Altmikus, M Kessler US Patent 9,174,728, 2015 | 68 | 2015 |
Aeroacoustic simulation of a complete H145 helicopter in descent flight U Kowarsch, C Öhrle, M Keßler, E Krämer Journal of the American Helicopter Society 61 (4), 1-13, 2016 | 45 | 2016 |
Aerodynamics and flight mechanics analysis of Airbus Helicopters’ compound helicopter RACER in hover under crosswind conditions J Thiemeier, C Öhrle, F Frey, M Keßler, E Krämer CEAS Aeronautical Journal 11, 49-66, 2020 | 40 | 2020 |
Tip vortex conservation on a helicopter main rotor using vortex-adapted chimera grids M Dietz, M Keßler, E Krämer, S Wagner AIAA journal 45 (8), 2062-2074, 2007 | 37 | 2007 |
Numerical investigations of dynamic stall on a rotor with cyclic pitch control J Letzgus, AD Gardner, T Schwermer, M Keßler, E Krämer Journal of the American Helicopter Society 64 (1), 1-14, 2019 | 32 | 2019 |
Computation of helicopter phenomena using a higher order method U Kowarsch, C Oehrle, M Hollands, M Keßler, E Krämer High Performance Computing in Science and Engineering ‘13: Transactions of …, 2013 | 29 | 2013 |
Higher-order simulations of a compound helicopter using adaptive mesh refinement C Öhrle, U Schäferlein, M Keßler, E Krämer Proceedings of the 74th Annual Forum of the American Helicopter Society …, 2018 | 28 | 2018 |
Compound helicopter X 3 in high-speed flight: correlation of simulation and flight test C Öhrle, F Frey, J Thiemeier, M Keßler, E Krämer, M Embacher, P Cranga, ... Journal of the American Helicopter Society 66 (1), 1-14, 2021 | 27 | 2021 |
Aerodynamic interactions on airbus helicopters' compound helicopter RACER in cruise flight F Frey, J Thiemeier, C Öhrle, M Keßler, E Krämer Journal of the American Helicopter Society 65 (4), 1-14, 2020 | 27 | 2020 |
Numerical assessment of open-rotor noise shielding with a coupled approach L Dürrwächter, M Keßler, E Krämer AIAA Journal 57 (5), 1930-1940, 2019 | 23 | 2019 |
Advances in parallelization and high-fidelity simulation of helicopter phenomena PP Kranzinger, U Kowarsch, M Schuff, M Keßler, E Krämer High Performance Computing in Science and Engineering´ 15: Transactions of …, 2016 | 23 | 2016 |
Coupled and trimmed aerodynamic and aeroacoustic simulations for Airbus Helicopters' compound helicopter RACER C Öhrle, F Frey, J Thiemeier, M Keßler, E Kräamer Journal of the American Helicopter Society 64 (3), 1-14, 2019 | 22 | 2019 |
Numerical investigation of helicopter rotors in ground effect B Kutz, U Kowarsch, M Kessler, E Kraemer 30th AIAA Applied Aerodynamics Conference, 2913, 2012 | 22 | 2012 |
High order CFD-simulation of the rotor-fuselage interaction U Kowarsch, M Keßler, E Krämer 39th European Rotorcraft Forum, Moscow, Russia, 2013 | 21 | 2013 |
Computational aeroacoustics with higher order methods ER Busch, MS Wurst, M Keßler, E Krämer High Performance Computing in Science and Engineering ‘12: Transactions of …, 2013 | 21 | 2013 |
Simulation of dynamic stall on an elastic rotor in high-speed turn flight J Letzgus, M Keßler, E Krämer Journal of the American Helicopter Society 65 (2), 1-12, 2020 | 20 | 2020 |
Trimmed simulation of a complete helicopter configuration using fluid-structure coupling M Dietz, M Kessler, E Krämer High Performance Computing in Science and Engineering07: Transactions of the …, 2008 | 20 | 2008 |
Advanced CFD-CSD coupling: Generalized, high performant, radial basis function based volume mesh deformation algorithm for structured, unstructured and overlapping meshes M Schuff, P Kranzinger, M Keßler, E Krämer | 19 | 2014 |