Klaus Hannemann

发表

German Test Facilities for High Speed Air Breathing Propulsion

Helmut Ciezki, Klaus Hannemann, O. Haidn, 2007 .

Master equation approach for modeling diatomic gas flows with a kinetic Fokker-Planck algorithm

Klaus Hannemann, Christian Hepp, Martin Grabe, 2020, J. Comput. Phys..

Numerical Study of Compressible Mixing Layers in Hyshot II Supersonic Combustor

Klaus Hannemann, Yancheng You, Heinrich Luedeke, 2011 .

Application of the Re-theta Transition Model in High Speed Flows

Thino Eggers, Klaus Hannemann, Heinrich Luedeke, 2012 .

Experimental and Numerical Analysis of the small Scale LAPCAT II Scramjet Flow Path in High Enthalpy Shock Tunnel Conditions

Johan Steelant, Klaus Hannemann, Sebastian Karl, 2014 .

Application of Temperature and Pressure Sensitive Paints to DLR Hypersonic Facilities: “lessons learned”

Ulrich Henne, Christian Klein, Klaus Hannemann, 2015 .

Hypersonic Flight and (Re)-Entry in Germany - Overview and Selected Projects

Klaus Hannemann, 2011 .

Modeling of H_2/O_2 Single-Element Rocket Thrust Chamber Combustion at Sub- and Supercritical Pressures with Different CFD Tools

Klaus Hannemann, Hendrik Riedmann, Daniel T. Banuti, 2015 .

The DLR Spacecraft Department – An Overview

Thino Eggers, Klaus Hannemann, 2011 .

Experimental Investigation of Supersonic Combustion in the HIEST and HEG Free Piston Driven Shock Tunnels

Klaus Hannemann, J. Martinez Schramm, T. Sunami, 2010 .

Study of MHD Effects in the High-Enthalpy Shock Tunnel Göttingen (HEG) Using a 30 T-Pulsed Magnet System

Klaus Hannemann, Jan Martinez Schramm, 2017 .

Aerothermodynamic Research in the Spacecraft Department of the German Aerospace Center : An Overview（グローバルAERO 海外空力機関訪問・滞在レポート第4回）

Thino Eggers, Klaus Hannemann, 啓伺小澤, 2013 .

An investigation into internal and external force balance configurations for short duration wind tunnels

Matthew Robinson, Klaus Hannemann, Jan Martinez Schramm, 2007 .

Experimental Investigation of Base Flow Buffeting on the ARIANE 5 Launcher Using High Speed PIV

Klaus Hannemann, Andrea Sciacchitano, Ferry Schrijer, 2011 .

High Enthalpy Hypersonic Aerothermodynamics and Space Propulsion Research at the DLR Spacecraft Department Göttingen

Klaus Hannemann, 2018 .

Force Measurement Using Non-Restrained Models in a Shock Tunnel

Masahiro Takahashi, Kazuo Sato, Kazuhisa Fujita, 2011 .

Numerical investigation of two interacting parallel thruster-plumes and comparison to experiment

Klaus Hannemann, Martin Grabe, André Holz, 2014 .

PRECISE – Preliminary results of the MEMS-based µCPS

Christopher Brunskill, Remco J. Wiegerink, Pelle Rangsten, 2013 .

Aerothermodynamics and Reentry

Klaus Hannemann, Jose Maria Longo, 2009 .

Numerical Validation of a Free-Flying Scramjet Powered Vehicle at Realistic Wind Tunnel Conditions

Johan Steelant, Klaus Hannemann, Sebastian Karl, 2014 .

Selected Research Activities and Future Fields of Interest at DLR Göttingen AS-RFZ

Klaus Hannemann, Alexander Wagner, 2019 .

CFD Analysis of the HyShot II Scramjet Experiments in the HEG Shock Tunnel

Andreas Mack, Johan Steelant, Klaus Hannemann, 2008 .

Ground testing of the HyShot supersonic combustion flight experiment in HEG

Johan Steelant, Klaus Hannemann, Anthony Donald Gardner, 2005 .

Hybrid RANS-LES Study of Transonic Flow in the Wake of a Generic Space Launch Vehicle

Klaus Hannemann, Kai Oßwald, Volker Hannemann, 2016 .

A Closely Coupled Experimental and Numerical Approach for Hypersonic and High Enthalpy Flow Investigations Utilising the HEG Shock Tunnel and the DLR TAU Code

Klaus Hannemann, Alexander Wagner, Sebastian Karl, 2010 .

Development of Temperature Sensitive Paints in the High Enthalpy Shock Tunnel Göttingen, HEG

Christian Klein, Klaus Hannemann, Hiroshi Ozawa, 2015 .

Computations of shock wave propagation with local mesh adaptation

Klaus Hannemann, Volker Hannemann, Bodo Reimann, 2009 .

Evaluation of full engine scramjet technology

Klaus Hannemann, Anthony Donald Gardner, 2004 .

Investigation of different modeling approaches for CFD simulation of high pressure rocket combustors

Klaus Hannemann, Sebastian Karl, Hendrik Riedmann, 2013 .

High Enthalpy Cylinder Flow in HEG: A Basis for CFD Validation

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2003 .

Experimental and Numerical Investigation of the HyShot II Flight Experiment

Klaus Hannemann, Sebastian Karl, Stuart J. Laurence, 2013 .

Recent Extensions to the High Enthalpy Shock Tunnel Göttingen (HEG

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2008 .

Force and Moment Measurements on a Free-Flying Capsule Model in a High-Enthalpy Shock Tunnel

Klaus Hannemann, Jan Martinez Schramm, Stuart J. Laurence, 2012 .

High Frequency Free-Stream Disturbance Measurements in Hypersonic Wind Tunnels by Means of a Slender Wedge Probe

Erich Schülein, Klaus Hannemann, Alexander Wagner, 2016 .

Interface advection with the TAU code and the CICSAM method on arbitrary grids

Klaus Hannemann, Markus Gauer, 2010 .

High Enthalpy Testing and CFD Rebuilding of X-38 in HEG

J.M.A. Longo, Klaus Hannemann, J. M. Schramm, 2001 .

High Enthalpy, High Pressure Short Duration Testing ofHypersonic Flows

Klaus Hannemann, Jan Martinez Schramm, J. Schramm, 2007 .

Application of the DLR TAU-Code to the RCM-1 Test Case: Penn State Preburner Combustor

Klaus Hannemann, Sebastian Karl, 2006 .

High enthalpy shock tunnel flow past a cylinder: A basis for CFD validation

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2004 .

LAPCAT Long-Term Advanced Propulsion Concepts and Technologies.Description of Model Geometry, Test Plan, Operating Conditions

Matthew Robinson, Klaus Hannemann, Judith Odam, 2006 .

CFD Investigation of Scaling Laws for Hydrogen Fuelled Scramjet Combustors

Johan Steelant, Klaus Hannemann, Sebastian Karl, 2008 .

Measurement of Aerodynamic Coefficients of Blunt Cones at the High Enthalpy Shock Tunnel Göttingen

Klaus Hannemann, Jan Martinez Schramm, Damian Friedl, 2016 .

Experimental determination of aerodynamic coefficients in rarefied environment based on the DLR-VxG lowdensitywind tunnels

Klaus Hannemann, Martin Grabe, Thomas Schlegat, 2016 .

Launch Vehicle Base Buffeting - Recent Experimental and Numerical Investigations

Klaus Hannemann, Heinrich Lüdeke, Fulvio Scarano, 2011 .

Transition Control for Hypersonic Flows - The Potential of Ultrasonically Absorptive TPSMaterials for Hypersonic Vehicles

Klaus Hannemann, Alexander Wagner, Markus Kuhn, 2016 .

Ground Testing Synthesis of the LAPCAT II Small Scale Flight Experiment Configuration Scramjet Flow Path

Sebastien Defoort, Johan Steelant, Klaus Hannemann, 2015 .

Proposals on Boundary Layer Transition by DLR AS-GÖ – Experimental Studies at HEG

Klaus Hannemann, Alexander Wagner, 2016 .

Design of a Flight Test Configuration for High-Speed Airbreathing Propulsion -Intermediate Review Phase 1

Klaus Hannemann, 2006 .

Ground Testing of the HyShot II Scramjet Configuration in HEG

Johan Steelant, Klaus Hannemann, Sebastian Karl, 2008 .

Steady Shock Refraction in Hypersonic Ramp Flow

Klaus Hannemann, Martin Grabe, Daniel T. Banuti, 2011 .

Conceptual Design of the High-Speed Propelled Experimental Flight Test Vehicle HEXAFLY

Johan Steelant, F. Di Matteo, Klaus Hannemann, 2015 .

Efficient multiphase rocket propellant injection model with high quality equation of state

Klaus Hannemann, Daniel T. Banuti, D. Banuti, 2014 .

ARD Post-Flight Analysis , Numerical Simulation and Experiments at HEG

Klaus Hannemann, J. Martinez Schramm, M. Weiland, 2001 .

Shock tunnel and numerical studies of a large inlet-fuelled inward turning axisymmetric scramjet

Russell R. Boyce, Klaus Hannemann, Jan Martinez Schramm, 2012 .

Aerothermodynamic Design of Space Vehicles: Experiment and CFD

J.M.A. Longo, Thino Eggers, Klaus Hannemann, 2003 .

26th International Symposium on Shock Waves

Klaus Hannemann, Friedrich Seiler, K. Hannemann, 2009 .

Contributions to the AVT-### / RTG on HYPERSONIC BOUNDARY-LAYER TRANSITION PREDICTION

Klaus Hannemann, Alexander Wagner, Viola Wartemann, 2013 .

High Enthalpy Non-Equilibrium Shock Layer Flows: Selected Practical Applications

Klaus Hannemann, Sebastian Karl, J. Martinez Schramm, 2012 .

Magnetic Fields and Ion Thruster Beam Effects in DLR’s EP Test Facility

Andreas Neumann, Klaus Hannemann, Nina Mühlich, 2016 .

Aerodynamic Testcases: DLR TAU Code

Klaus Hannemann, Jan Martinez Schramm, Damian Friedl, 2015 .

Hypersonic Research in the High-Enthalpy Shock Tunnel Göttingen

Klaus Hannemann, 2017 .

The New DLR High Vacuum Test Facility STG-ET

Klaus Hannemann, Andreas Neumann, Hans-Peter Harmann, 2011 .

Hypersonic and Space Propulsion Research at the DLR Spacecraft Department Göttingen

Klaus Hannemann, 2018 .

Validation study of numerical simulations by comparison to measurements in piston-driven shock-tunnels

Peter A. Jacobs, Russell R. Boyce, Klaus Hannemann, 2007 .

Post flight analysis of SHEFEX I: Shock tunnel testing and related CFD analysis

Klaus Hannemann, Alexander Wagner, Andreas Schröder, 2009 .

Numerical and Experimental Analysis of Low-Density Effects in Suborbital Flight of FAST20XX

Klaus Hannemann, Raffaele Votta, Marco Marini, 2012 .

Technological Step Stones in Support to Future Space Transportation Systems

Klaus Hannemann, Jose Maria Longo, 2008 .

Comparative Analysis of CFD and PIV Base Buffeting Data Considering Decomposition Techniques and Filtering Effects in the Measurement Chain

Klaus Hannemann, Tim Horchler, Paul Blinde, 2015 .

Validation of the DLR TAU Code for Scale-Resolving Combustion Simulations

Klaus Hannemann, Tim Horchler, Stefan Fechter, 2018 .

Experimental study of plume flow emanating from rectangular orifices

Klaus Hannemann, Martin Grabe, Ellen Werner, 2014 .

New 2d Far Field Beam Scanning Device at DLR's Electric Propulsion Test Facility

Klaus Hannemann, Andreas Neumann, Peter J. Klar, 2015 .

Comparison of Decoupled Hybrid Navier-Stokes - DSMC Calculations with Experiments in Plumes

Klaus Hannemann, Mathis Rosenhauer, Klaus Plahn, 1999 .

High Enthalpy Flows in the HEG Shock Tunnel: Experiment and Numerical Rebuilding (Invited)

Klaus Hannemann, K. Hannemann, 2003 .

Aerothermodynamics of the ARD: Postflight Numerics and Shock-Tunnel Experiments

J.M.A. Longo, Klaus Hannemann, J. Martinez Schramm, 2002 .

Combustion Experiments Performed within the LAPCAT I Project - An Overview

Andreas Mack, Johan Steelant, Helmut Ciezki, 2009 .

Application of the DLR TAU-Code to the RCM-4 Test Case: Microcombustor Ignition

Klaus Hannemann, Sebastian Karl, 2006 .

Investigation of Hypersonic Boundary-Layer Transition Using High-Speed Visualization Techniques

Klaus Hannemann, Stuart J. Laurence, Alexander Wagner, 2013 .

Flow control by energy deposition in hypersonic flow - some fundamental considerations

Klaus Hannemann, Daniel T. Banuti, 2009 .

Overview of the research activities of the RITSAT-project

Klaus Hannemann, Ubbo Ricklefs, Hans Leiter, 2015 .

Application of a Real-Gas-Library Multi-Fluid-Mixing Model to Supercritical Single Injector Flow

Klaus Hannemann, Daniel T. Banuti, D. Banuti, 2014 .

Modifications to the DLR High Enthalpy Shock Tunnel HEGfor Measurements on Supersonic Combustion

Klaus Hannemann, Walter Beck, Matthias Weiland, 2001 .

Shock tunnel free flight force measurements using a complex model configuration

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2015 .

Application of HEG static pressure probe in HIEST

Matthew Robinson, Klaus Hannemann, Tomoyuki Komuro, 2009 .

Free Flight Testing of a Scramjet Engine in a Large Scale Shock Tunnel

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2015 .

Free-flight force measurement technique in a shock tunnel

Masahiro Takahashi, Kazuo Sato, Kazuhisa Fujita, 2012 .

Design of a Flight Configuration for High Speed Airbreathing PropulsionIdentification of the Flight Test Programm

Klaus Hannemann, 2006 .

Design and Optimization of a Small Scale M=8 Scramjet Propulsion System

Klaus Hannemann, Sebastian Karl, Tobias Langener, 2012 .

Selected Supersonic Combustion Activities at DLR within the European LAPCAT Project

Klaus Hannemann, Oskar Haidn, Helmut Ciezki, 2007 .

Efficient Analysis of Transonic Base Flows Employing Hybrid RANS/LES Methods

Klaus Hannemann, Th. Eggers, V. Hannemann, 2017 .

Aerothermal Analysis of Reusable First Stage Launcher during Re-Entry Retro-Propulsion

Klaus Hannemann, Etienne Dumont, Tobias Ecker, 2017 .

Experimental Comparative Synthesis on the Scramjet Powered Waverider Vehicle in HEG and F4 within the LAPCAT II project

Sebastien Defoort, Johan Steelant, Klaus Hannemann, 2015 .

Rarefied Aerothermodynamics Technology Development for Future High-Altitude High-Speed Transport (EU-FAST20XX)

Klaus Hannemann, Martin Sippel, Raffaele Votta, 2013 .

Combined Experimental and Numerical Characterization of the HEG Test Section Flow

Klaus Hannemann, M. Schnieder, B. Reimann, 1999 .

Investigation of different modeling approaches for computational fluid dynamics simulation of high-pressure rocket combustors

Klaus Hannemann, Manuel Frey, Blazenko Ivancic, 2016 .

Measurements by Means of Optical Tracking in the High Enthalpy Shock Tunnel Göttingen, HEG

Klaus Hannemann, Jan Martinez Schramm, Damian Friedl, 2015 .

Achievements Obtained for Sustained Hypersonic Flight within the LAPCAT project.

Sebastien Defoort, Johan Steelant, Klaus Hannemann, 2008 .

Planar Micro Nozzles - CFD Model Demands for Thrust Optimization

Klaus Hannemann, Martin Grabe, Daniel T. Banuti, 2014 .

Balance Configurations for Short Duration Wind Tunnels

Klaus Hannemann, Jan Martinez Schramm, Matthew Robinson, 2007 .

Joint European Effort Towards Advanced Rocket Thrust Chamber Technology

Ralf Stark, Klaus Hannemann, Luca Boccaletto, 2005 .

Comparison of Computed Free Thruster PlumeExpansion to Experiments

Klaus Hannemann, Martin Grabe, Georg Dettleff, 2014 .

DLR's Electric Propulsion Test Facility - the First Three Years of Thruster Operation

Andreas Neumann, Klaus Hannemann, Stefan Stämm, 2015 .

End-to-end modelling and design of a new operating condition for HEG

Peter A. Jacobs, Klaus Hannemann, Anthony Donald Gardner, 2004 .

Test Case 1a: Short Nozzle Under Separated Flow Condition – Numerical Investigation with the DLR Tau-Code

Bernd Wagner, Klaus Hannemann, Sebastian Karl, 2006 .

Aspects of thermal flow control in hypersonic flight

Klaus Hannemann, Daniel T. Banuti, Jose Maria Longo, 2010 .

Sensitivity Analysis for the HyShot Generic Supersonic Combustion Configuration using CFD

Andreas Mack, Klaus Hannemann, Jan Martinez Schramm, 2007 .

Flow Characteristics of Micro-Scale Planar Nozzles

Klaus Hannemann, Martin Grabe, Daniel T. Banuti, 2014 .

Layout and Design Verification of a Small Scale Scramjet Combustion Chamber

Johan Steelant, Klaus Hannemann, Sebastian Karl, 2013 .

DLR Spacecraft Department Göttingen - Research Fields, Infrastructure and selected Research Activities

Klaus Hannemann, 2019 .

グルーバルAERO 海外空力機関訪問・滞在レポート Aerothermodynamic Research in the Spacecraft Department of the German Aerospace Center : An Overview

Thino Eggers, Klaus Hannemann, 小澤啓伺, 2013 .

Evaluation of full -engine scramjet technology. Executive Summary

Klaus Hannemann, Anthony Donald Gardner, 2004 .

A Computational Study of the HySHOT II Combustor Performance

Klaus Hannemann, Christer Fureby, Sebastian Karl, 2013 .

Electric Propulsion Testing at the DLR Göttingen: Facility and Diagnostics

Andreas Neumann, Klaus Hannemann, 2014 .

Free Piston Shock Tunnels HEG, HIEST, T4 and T5

Hans G. Hornung, Klaus Hannemann, Katsuhiro Itoh, 2016 .

Comparison of supersonic combustion tests with shock tunnels, flight and CFD

Andreas Mack, Johan Steelant, Klaus Hannemann, 2006 .

Extrapolation of a Generic Scramjet Model to Flight Scale by Experiments, Flight Data and CFD

Andreas Mack, Johan Steelant, Klaus Hannemann, 2009 .

CFD Analysis of the Hyshot Combustion Flight Experiment Configuration

Andreas Mack, Johan Steelant, Klaus Hannemann, 2006 .

Status of the High Enthalpy Shock Tunnel HEG at the DLR Göttingen

Klaus Hannemann, Walter Beck, M. Schnieder, 1999 .

Investigation of the ARD Aerothermodynamics at DLR: An Overview

J.M.A. Longo, Klaus Hannemann, M. Weiland, 2001 .

Post Flight Experiments of the SHEFEX I Configurationin the High Enthalpy Shock Tunnel Göttingen (HEG)

Klaus Hannemann, Alexander Wagner, Jan Martinez Schramm, 2009 .

CFD Analysis of the HyShot Supersonic Combustion Flight Experiment Configuration

Andreas Mack, Johan Steelant, Klaus Hannemann, 2006 .

Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor. Part I: Shock-tunnel experiments

Klaus Hannemann, Stuart J. Laurence, J. Martinez Schramm, 2015 .

Investigation of Structured and Unstructured Grid Topology and Resolution Dependence for Scale-Resolving Simulations of Axisymmetric Detaching-Reattaching Shear Layers

Klaus Hannemann, Volker Hannemann, Jan-Erik Schumann, 2019, Progress in Hybrid RANS-LES Modelling.

An Experimental Investigation of Steady and Unsteady Combustion Phenomena in the HyShot II Combustor

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2011 .

Injection and mixing in a scramjet combustor: DES and RANS studies

Klaus Hannemann, Yancheng You, Y. You, 2013 .

Experimental investigation of different scramjet hydrogen injection systems

Klaus Hannemann, K. Hannemann, 2008 .

Aerothermal Analysis of Reusable Launcher Systems during Retro-Propulsion Reentry and Landing

Klaus Hannemann, Sebastian Karl, Tobias Ecker, 2018 .

Investigation of Unsteady/Quasi-Steady Scramjet Behavior using High-Speed Visualization Techniques

Klaus Hannemann, Hiroshi Ozawa, Jan Martinez Schramm, 2012 .

Numerical Simulation of Liquid Rocket Engine Cooling Channels

Javier Bartolome Calvo, Klaus Hannemann, K. Hannemann, 2009 .

On the flow physics of a low momentum flux ratio jet in a supersonic turbulent crossflow

Klaus Hannemann, Heinrich Lüdeke, Yancheng You, 2012 .

Analysis of the Heat Transfer in Liquid Rocket Engine Cooling Channels

Klaus Hannemann, J. Bartolome Calvo, 2010 .

Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG and Comparison with Flight Data (AIAA 2004–3345)

Johan Steelant, Allan Paull, Klaus Hannemann, 2004 .

Time-Resolved Visualization of Instability Waves in a Hypersonic Boundary Layer

Klaus Hannemann, Alexander Wagner, Heinrich Lüdeke, 2012 .

Cylinder Shock Layer Density Profiles Measured in High Enthalpy Flows in HEG

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2002 .

MIXING AND COMBUSTION ENHANCEMENT IN A GENERIC SCRAMJET COMBUSTION CHAMBER

Andreas Mack, Johan Steelant, Klaus Hannemann, 2006 .

High Speed Flow Visualization at HEG

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2004 .

Blunt body near-wake flow field at Mach 10

Thomas J. Horvath, Klaus Hannemann, T. Horvath, 1997 .

Sonic Line and Stand–Off Distance on Re–entry Capsule Shapes

Hans G. Hornung, Klaus Hannemann, Jan Martinez Schramm, 2012 .

Short duration force measurements in impulse facilities

Klaus Hannemann, K. Hannemann, Matthew Robinson, 2006 .

The influence and the delay of driver gas contamination in HEG

Klaus Hannemann, M. Schnieder, M. Schnieder, 2000 .

Mixing and Combustion Enhancement in a Generic Combustion Chamber

Andreas Mack, Johan Steelant, Klaus Hannemann, 2006 .

Launch Vehicle Base Flow Analysis Using Improved Delayed Detached-Eddy Simulation

Klaus Hannemann, Heinrich Lüdeke, Jean Daniel Mulot, 2015 .

Real Gas Library in Continuous Phase Propellant Injection Model for Liquid Rocket Engines

Klaus Hannemann, Daniel T. Banuti, D. Banuti, 2013 .

CFD Analysis of Unstart Characteristics of the HyShot II Scramjet Configuration in the HEG Shock Tunnel

Klaus Hannemann, Sebastian Karl, Jan Martinez Schramm, 2011 .

Understanding scramjet combustion using LES of the HyShot II combustor

Klaus Hannemann, Christer Fureby, Sebastian Karl, 2017 .

Time resolved holographic interferometry for short duration hypersonic high enthalpy test facilities

Klaus Hannemann, J. Martinez Schramm, A. Boutry, 2005 .

Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths

Johan Steelant, Klaus Hannemann, Sebastian Karl, 2010 .