| Transient fluid-combustion phenomena in a model scramjet SJ Laurence, S Karl, JM Schramm, K Hannemann Journal of Fluid Mechanics 722, 85-120, 2013 | 146 | 2013 |
| Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor. Part I: Shock-tunnel experiments SJ Laurence, D Lieber, JM Schramm, K Hannemann, J Larsson Combustion and Flame 162 (4), 921-931, 2015 | 105 | 2015 |
| A computational study of the HyShot II combustor performance M Chapuis, E Fedina, C Fureby, K Hannemann, S Karl, JM Schramm Proceedings of the Combustion Institute 34 (2), 2101-2109, 2013 | 80 | 2013 |
| Fast-response temperature-sensitive-paint measurements on a hypersonic transition cone H Ozawa, SJ Laurence, JM Schramm, A Wagner, K Hannemann Experiments in Fluids 56 (1), 1853, 2015 | 78 | 2015 |
| Experiments on passive hypersonic boundary layer control using ultrasonically absorptive carbon–carbon material with random microstructure A Wagner, M Kuhn, J Martinez Schramm, K Hannemann Experiments in Fluids 54, 1-10, 2013 | 75 | 2013 |
| Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths K Hannemann, S Karl, J Martinez Schramm, J Steelant Shock Waves 20, 353-366, 2010 | 72 | 2010 |
| High enthalpy cylinder flow in HEG: A basis for CFD validation S Karl, J Martinez Schramm, K Hannemann 33rd AIAA Fluid Dynamics Conference and Exhibit, 4252, 2003 | 69 | 2003 |
| Recent extensions to the high enthalpy shock tunnel Göttingen (HEG) K Hannemann, J Martinez Schramm, S Karl Proceedings of the 2nd International ARA Days “Ten Years after ARD …, 2008 | 68 | 2008 |
| Ground testing of the HyShot II scramjet configuration in HEG JM Schramm, S Karl, K Hannemann, J Steelant AIAA paper 2547, 2008, 2008 | 53 | 2008 |
| Application of particle image velocimetry and the background-oriented schlieren technique in the high-enthalpy shock tunnel Göttingen T Kirmse, J Agocs, A Schröder, J Martinez Schramm, S Karl, ... Shock waves 21, 233-241, 2011 | 51 | 2011 |
| Design and implementation of an internal stress wave force balance in a shock tunnel MJ Robinson, J Martinez Schramm, K Hannemann CEAS Space Journal 1, 45-57, 2011 | 48 | 2011 |
| An experimental investigation of steady and unsteady combustion phenomena in the HyShot II combustor S Laurence, J Martinez Schramm, S Karl, K Hannemann 17th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2011 | 46 | 2011 |
| Cylinder shock layer density profiles measured in high enthalpy flows in HEG J Martinez Schramm, K Hannemann, W Beck, S Karl 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2913, 2002 | 35 | 2002 |
| STRATOFLY MR3–how to reduce the environmental impact of high-speed transportation N Viola, R Fusaro, O Gori, M Marini, P Roncioni, G Saccone, B Saracoglu, ... AIAA Scitech 2021 Forum, 1877, 2021 | 32 | 2021 |
| High enthalpy, high pressure short duration testing of hypersonic flows K Hannemann, J Martinez Schramm Springer handbook of experimental fluid mechanics, 1081-1125, 2007 | 31 | 2007 |
| Development of Temperature Sensitive Paints in the High Enthalpy Shock Tunnel Göttingen, HEG J Martinez Schramm, K Hannemann, H Ozawa, W Beck, C Klein | 30* | 2015 |
| The high enthalpy shock tunnel Göttingen of the German aerospace center (DLR) K Hannemann, J Martinez Schramm, A Wagner, G Ponchio Camillo Journal of large-scale research facilities JLSRF 4 (A133), 1-14, 2018 | 29 | 2018 |
| Investigation of unsteady/quasi-steady scramjet behavior using high-speed visualization techniques S Laurence, H Ozawa, D Lieber, J Martinez Schramm, K Hannemann 18th AIAA/3AF International Space Planes and Hypersonic Systems and …, 2012 | 29 | 2012 |
| Visualization of hypersonic boundary-layer transition on a slender cone SJ Laurence, A Wagner, H Ozawa, K Hannemann 19th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2014 | 28 | 2014 |
| A closely coupled experimental and numerical approach for hypersonic and high enthalpy flow investigations utilising the HEG shock tunnel and the DLR TAU code K Hannemann, JM Schramm, A Wagner, S Karl, V Hannemann VKI/RTO Lecture Series, RTO-EN-AVT-186 Aerothermodynamic Design, Review on …, 2010 | 27 | 2010 |
