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Dr. Jan Martinez Schramm
Dr. Jan Martinez Schramm
Bestätigte E-Mail-Adresse bei dlr.de - Startseite
Titel
Zitiert von
Zitiert von
Jahr
Transient fluid-combustion phenomena in a model scramjet
SJ Laurence, S Karl, JM Schramm, K Hannemann
Journal of Fluid Mechanics 722, 85-120, 2013
1462013
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
1052015
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
802013
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
782015
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
752013
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
722010
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
692003
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
682008
Ground testing of the HyShot II scramjet configuration in HEG
JM Schramm, S Karl, K Hannemann, J Steelant
AIAA paper 2547, 2008, 2008
532008
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
512011
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
472011
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
462011
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
352002
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
322021
High enthalpy, high pressure short duration testing of hypersonic flows
K Hannemann, J Martinez Schramm
Springer handbook of experimental fluid mechanics, 1081-1125, 2007
312007
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
292018
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
292012
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
282014
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
272010
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