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Stephan Maria Hitzel

Observed names: Hitzel, Stephan, Hitzel, Stephan M., S. HITZEL, S. Hitzel, S. M. Hitzel, STEPHAN HITZEL, Stephan Hitzel, Stephan M. Hitzel
OpenAlex ID: A5108771443
Flow Physics Analyses of a Generic Unmanned Combat Aerial Vehicle Configuration
2012 · Andreas Schütte, Dietrich Hummel, et al. · Journal of Aircraft · 85
Numerical and experimental analyses of the vortical flow around the SACCON configuration
2010 · Andreas Schuette, Dietrich Hummel, et al. · AIAA Applied Aerodynamics Conference · 72
Slender wings with leading-edge vortex separation - A challenge for panel methods and Euler solvers
1984 · Stephan M. Hitzel, Wolfgang Schmidt · Journal of Aircraft · 59
Validation of numerical prediction of dynamic derivatives: The DLR-F12 and the Transcruiser test cases
2011 · Bruno Mialon, Alex Khrabrov, et al. · Progress in Aerospace Sciences · 31
Wing vortex-flows up into vortex breakdown - A numerical simulation
1988 · STEPHAN HITZEL · AIAA Applied Aerodynamics Conference · 26
Parallel remeshing of unstructured volume grids for CFD applications
2006 · U. Tremel, K. A. Sørensen, et al. · International Journal for Numerical Methods in Fluids · 25
Enhanced Maneuverability of a Delta-Canard Combat Aircraft by Vortex Flow Control
2017 · Stephan Maria Hitzel, Robert Osterhuber · Journal of Aircraft · 22
Vortex development on the AVT-183 diamond wing configuration – numerical and experimental findings
2015 · Stephan Maria Hitzel, Okko Joost Boelens, et al. · Aerospace Science and Technology · 22
JDAM-Store Separation from an F/A-18C - An Application of the Multidisciplinary SimServer-System
2005 · Udo Tremel, Stephan Hitzel, et al. · AIAA Applied Aerodynamics Conference · 18
Vortex Flows of the F-16XL Configuration - CAWAPI-II Free-Flight Simulations
2014 · Stephan M. Hitzel · AIAA Aerospace Sciences Meeting · 16
Status of CFD validation on the vortex flow experiment
1988 · Bernhard Wagner, Stephan M. Hitzel, et al. · 15
Sub- and Transonic Vortex Breakdown Flight Condition Simulations of the F-16XL Aircraft
2015 · Stephan Hitzel · Journal of Aircraft · 13
Vortex Development on the AVT-183 Diamond Wing Configuration - Numerical and Experimental Findings
2015 · Stephan M. Hitzel, Okko J. Boelens, et al. · AIAA Aerospace Sciences Meeting · 13
Simulation of Manoeuvring Aircraft with the Unstructured Chimera Approach
2007 · Kaare Sorensen, Udo Tremel, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 13
Model Scale and "Real" Flight of Generic UCAV and Advanced Combat Aircraft - An Industrial Perspective
2014 · Stephan M. Hitzel, Dirk Zimper · AIAA Applied Aerodynamics Conference · 11
European Benchmark on Numerical Prediction of Stability and Control derivatives
2009 · Bruno Mialon, Saloua Ben Khelil, et al. · AIAA Applied Aerodynamics Conference · 11
Vortex Flow Aerodynamic Challenges in the Design Space for Future Fighter Aircraft
2019 · Stephan M. Hitzel, Andreas Winkler, et al. · Notes on numerical fluid mechanics and multidisciplinary design · 10
High-Angle-of-Attack F-16XL Flight Simulations at Sub- and Transonic Speeds
2017 · Stephan Hitzel · Journal of Aircraft · 10
Analysis of Vortex Flow Phenomena on Generic Delta Wing Planforms at Transonic Speeds
2019 · Andreas Hövelmann, Andreas Winkler, et al. · Notes on numerical fluid mechanics and multidisciplinary design · 8
Synthesis of Hybrid Computational Fluid Dynamics Results for F-16XL Aircraft Aerodynamics
2017 · James M. Luckring, Michael A. Park, et al. · Journal of Aircraft · 8
Program Overview: Vortex Interaction Aerodynamics Relevant to Military Air Vehicle Performance
2022 · James M. Luckring, Nigel J. Taylor, et al. · AIAA SciTech Forum · 6
Hybrid-Delta Wing Simulations – Industrial Application for Combat Aircraft Design
2022 · Andreas Hövelmann, Patrick Pölzlbauer, et al. · AIAA SciTech Forum · 5
Wind Tunnel, Simulation, and “Real” Flight of Advanced Combat Aircraft: Industrial Perspective
2016 · Stephan Hitzel, Dirk Zimper · Journal of Aircraft · 5
modeFRONTIER©, a Framework for the Optimization of Military Aircraft Configurations
2009 · L. Nardin, K. Sørensen, et al. · Notes on numerical fluid mechanics and multidisciplinary design · 5
Slender wings with leading-edge vortex separation - A challenge for panel-methods and Euler-solvers
1983 · S. HITZEL, W. SCHMIDT · AIAA Aerospace Sciences Meeting · 5
Works count: 47
Citation count: 545
H-index: 13
I10-index: 18
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