Veröffentlichungen und Vorträge

 
 
 
 
  
 
 
Benjamin Spiess, Klaus Höschler, Maren Fanter
Using a smart recognition framework for the automated transfer of geometry to whole engine mechanical models
Stefan Kazula, Klaus Höschler
Review of variable leading edge patents for aircraft wings and engine inlets and their relevance for variable pitot inlets in future supersonic transport, CEAS Aeronautical Journal, 2021
Stefan Kazula, Beatrice Rich, Klaus Höschler und Ralf  Woll
Interest High School Students in STEM Studies, while Preparing
STEM Students for Leading Positions In: 2021 IEEE Global Engineering Education Conference (EDUCON) EDUCON)

2021 IEEE Global Engineering Education Conference (EDUCON) EDUCON): IEEE, 2021, S. 910
Tianxiao Xie, Tommy Starick, Anatol Mosgow, Heinz Peter Berg , Klaus Höschler
Thermofluiddynamic pre-design of a primary surface heat exchanger under the influence of heat radiation using 1D/3D coupled simulation method
NAFEMS World Congress
Benjamin Spieß, K. Höschler, Maren Fanter
DEVELOPMENT OF A SIMULATION-BASED KNOWLEDGE REPRESENTATION FOR THE SIMPLIFICATION OF STRUCTURAL AERO ENGINE COMPONENTS
NAFEMS World Congress
Stefan Kazula, K. Höschler
Variable Pilot-Triebwerkseinlässe für kommerzielle Überschallflugzeuge
Konzeptstudie mittels eines Entwicklungsansatze für sichere Produkte, Springer Verlag DOI: 10.1007/978-3-658-35456-5
 
 
 
Stefan Kazula, Klaus Höschler
Ice detection and protection systems for circular variable nacelle inlet concepts
CEAS Aeronautical Journal, 2020, 11(1), 229-248. ISSN 1869-5582. DOI:10.1007/s13272-019-00413-1
Stefan Kazula, Klaus Höschler
Evaluation of variable pitot inlet concepts for transonic and supersonic civil aviation
Aircraft Engineering and Aerospace Technology, 2020, 92(6), 807-815. ISSN 1748-8842. DOI:10.1108/AEAT-11-2019-0225
Stefan Kazula, Mark Wöllner, Klaus Höschler
Identification of efficient geometries for variable pitot inlets for supersonic transport
Aircraft Engineering and Aerospace Technology, 2020, 92(7), 981-992. ISSN 1748-8842. DOI:10.1108/AEAT-11-2019-0228
Stefan Kazula, Klaus Höschler
Review of Variable Leading Edge Patents for Aircraft Wings and Engine Inlets and Their Relevance for Variable Pitot Inlets in Future Supersonic Transport
Deutscher Luft- und Raumfahrtkongress 2020, Online, 1. bis 3. September 2020
Stefan Kazula, Klaus Höschler
A Variable Pitot Inlet Concept for Supersonic Aviation
Proceedings of Global Power and Propulsion Society GPPS Chania20, 2020. DOI: 10.33737/gpps20-tc-49
Tolga Yagci, Klaus Höschler, Stephan Pannier, Sven von Ende
Proceedings IRF2020 7th International Conference Integrity Reliability  Failure
Funchal/Portugal 14-18 June 2020 Edilors J-F. Silva Gomes and S.A. Meguid, Publ. INEGI/FEUP (2020), ISBN:978-989-20-8315-3
 
Marcel Mischke, Michael Pohl, Klaus Höschler, André Huppertz
A Holistic Approach for the Generic Preliminary Design of Axial Compressor and Turbine Annulus Contours
Deutscher Luft- und Raumfahrtkongress 2020, Bonn DGLR 2020, Conference Paper, DOI: 10.25967/530097
Marcel Mischke, Michael Pohl, Klaus Höschler, André Huppertz
GAS PATH DESIGNER – zeiteffiziente Vorauslegung von Triebwerks-Ringräumen und zusätzlichen Strukturen
Deutscher Luft- und Raumfahrtkongress 2020, Bonn DGLR 2020, Conference Paper, DOI: 10.25967/530098  
Paul König, Marcel Mischke, Michael Pohl, Stefan Kazula, Klaus Höschler
Concept Development and Evaluation for a Broadband Noise Absorbing Acoustic Liner Concept for Aviation
24th International Society For Air Breathing Engines (ISABE-2019-24261), 22.-27. September 2019
Stefan Kazula, Mark Wöllner, David Grasselt, Klaus Höschler
Ideal Geometries and Potential Benefit of Variable Pitot Inlets for Subsonic and Supersonic Business Aviation
8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Stefan Kazula, Mark Wöllner, David Grasselt, Klaus Höschler
Parametric Design and aerodynamic analysis of circular variable aero engine inlets for Transonic and Supersonic Aviation
Proceedings of the 24th ISABE Conference
Stefan Kazula, Marcel Mischke, Klaus Höschler
Evaluation of Variable Pitot Inlet Concepts for Transonic and Supersonic Civil Aviation
Proceedings of the 9th EASN International Conference on Innovation in Aviation & Space
Stefan Kazula, Mark Wöllner, David Grasselt, Klaus Höschler
Parametric Design Study on Aerodynamic Characteristics of Variable Pitot Inlets for Transonic andSupersonic Aviation
Proceedings of the 9th EASN International Conference on Innovation in Aviation & Space
Stefan Kazula, Klaus Höschler
Ice detection and protection systems for circular variable nacelle inlet concepts
CEAS Aeronautical Journal
Stefan Kazula, Klaus Höschler
A systems engineering approach to variable intakes for civil aviation
Proceedings of the Institution of Mechanical Engineers. Part G, Journal of Aerospace Engineering
Marcel Mischke, Stefan Kazula, Klaus Höschler
A Comparative Concept Study and Evaluation for New Broadband Noise Absorbing Acoustic Liner Concepts for Civil Aviation
Proceedings of Global Power and Propulsion Society, Technical Conference 2019, Zurich
Marcel Mischke, Stefan Kazula, Klaus Höschler
Preliminary safety Assessment on System Design Level for Broadband Acoustic Liner Concepts for Aviation
Proceedings of the 9th EASN International Conference on Innovation in Aviation & Space,
MATEC Web Conf.Volume 304, 2019, DOI:org/10.1051/matecconf/201930404010
Beya Mhadbi, Marcel Mischke, Klaus Höschler, Andre Huppertz
Semi-automatische Erstellung parametrisch-assoziativer 3D CAD-Modelle am Beispiel eines Flug-Kerntriebwerks, Digitalisierung und Produktentwicklung - vernetzte Entwicklungsumgebungen
16. Gemeinsames Kolloquium Konstruktionstechnik 2018, Bayreuth, Tagungsband, S. 236 - 243
Toni Wildow, Klaus Höschler, Hubert Dengg, Jonathan Sommerfeld
Adaptive Preliminary-Design workflow for aero engine Secondary Air system cavities with an application case of windage and heat transfer in a rotor-stator cavity with axial throughflow
Proceedings of ASME Turbo Expo 2018 (GT2018-76201), June 2018, Oslo (Norway)
Stefan Kazula, David Grasselt, Klaus Höschler
Preliminary safety assessment of circular variable nacelle inlet concepts for aero engines in civil aviation
Safety and Reliability – Safe Societies in a Changing World, S. 2459 – 2467, 2018, London : Taylor & Francis Group
Stefan Kazula, David Grasselt, Klaus Höschler
Common cause analysis of circular variable nacelle inlet concepts for aero engines in civil aviation
Proceedings IRF2018: 6th International Conference Integrity-Reliability-Failure, Lisbon/Portugal, 22-26 July 2018, S. 759 - 770
Stefan Kazula, Klaus Höschler
Ice detection and protection systems for circular variable nacelle inlet concepts
Deutscher Luft- und Raumfahrtkongress 2018, Friedrichshafen, 4. bis 6. September 2018, S. 1 - 15
Klaus Hoeschler, E. Sarradj, N. Modler, L. Enghardt
Novel jet engine acoustic liner with improved broadband noise absorption
31st Congress of the International Council of the Aeronautical Sciences (ICAS)
19 - 24 September 2018 Belo Horizonte, Brasilien
Stefan Kazula, Beatrice Rich, Klaus Höschler, Ralf Woll
Awakening the Interest of High School Pupils in Science, Technology, Engineering and Mathematics Studies and Careers through Scientific Projects
2018 International Conference on Teaching, Assessment, and Learning for Engineering (TALE), 4-7 December 2018, Wollongong, NSW, Australia, S. 259 - 265
Chetan Kumar Sain, Klaus Höschler
Comparative Assessment between Variable Area Fan Nozzle Concepts at Inner and Outer By-Pass Duct Surfaces
23rd International Symposium on Air Breathing Engines (ISABE-2017-21342), 03.-08. September 2017, Manchester (UK)
David Grasselt, Klaus Höschler, Stefan Kazula
A Design Approach for a Coupled Actuator System for Variable Nozzles and Thrust Reverser of Aero Engines
ISABE 2017 Conference, 3-8 September 2017, Manchester (UK)
David Grasselt, Klaus Höschler, Chetan Kumar Sain
Fluid-Structure Interaction With a Fully Integrated Multiphysics Environment
ASME 2017 Fluids Engineering Division Summer Meeting (DOI: 10.1115/FEDSM2017-69078), Waikoloa, Hawaii, USA, July 30–August 3, 2017
Chetan Kumar Sain, Klaus Höschler
Aerodynamic Assessment of Nozzle Area Variation by Core Fairing Modulation
CEAS Aeronautical Journal 253 (DOI: 10.1007/s13272-017-0253-4), 28.06.2017
Stefan Kazula, Höschler, Klaus Höschler
A Systems Engineering Approach to Variable Intakes for Civil Aviation
7th European Conference for Aero Nautics and Space Sciences (EUCASS), Milan (Italien), 2017
David Grasselt, Klaus Höschler
Safety Assessment of Aero Engine Thrust Reverser Actuation Systems
22nd International Symposium on Air Breathing Engines (ISABE-2015-20260), 25.-30. Oktober 2015, Phoenix (AZ, USA)
David Grasselt, Klaus Höschler
Vergleich von FSI Methoden kommerzieller integrativer Programme gegenüber inkonsistenten Lösungen am Beispiel eines Schubumkehrers im Flug-Triebwerk
Deutscher Luft- und Raumfahrtkongress (DLRK), 22.-24. September 2015, Rostock
Chetan Kumar Sain, Klaus Höschler, Marcel Mischke
Concept study of variable area fan nozzle for UHBPR turbofan engine
22nd International Symposium on Air Breathing Engines (ISABE-2015-20260), 25.-30. Oktober 2015, Phoenix (AZ, USA)
Chetan Kumar Sain, Klaus Höschler
Aerodynamic Assessment of Nozzle Area Variation by Core Fairing Modulation
Deutscher Luft- und Raumfahrtkongress (DLRK), 22.-24. September 2015, Rostock
David Grasselt, Klaus Höschler, Aris Konstantinidis
Fluid Structure Interaction with Inconsistent Software Platforms
ECCOMAS , Juli 20 - 25 2014 Barcelona
H. Schlums, D.S. Tchankov, K. Höschler, U. Müller
Crack Initiation Life Predictions for Notched Specimen Based on Chaboche Deformation Model
6th International Conference on Engineering Structural Integrity Assessment, Manchester (Großbritannien), Oktober 2002
M. Gerendás, K. Höschler, T. Schilling
Development and Modelling of Angled Effusion Cooling for the BR715 Low Emission Staged Combustor Core Demonstrator
NATO RTO Symposium on Advanced Flow Management, Loen (Norwegen), Mai 2001
K. Höschler, J. Bishof, W. Koschel
Thermo-mechanical Analysis of an Automotive Diesel Engine Exhaust Manifold
SF2M Temperature-Fatigue Interaction, Paris (Frankreich), Mai 2001
KU. Müller, K. Höschler, M. Gerendás, H.-J. Bauer, U. Schoth
Mechanical Analysis of an Aero-Engine Combustor under Operation Conditions using a Unified Constitutive Material Model for Deformation Simulation
SF2M Temperature-Fatigue Interaction, Paris (Frankreich), Mai 2001
K. Höschler, A. Schmid, U. Müller, H.-J. Bauer
Life Assessment of a Jet Engine Combustor Liner Support Feature under Consideration of Casing Flange Deformation
NAFEMS-Seminar Fatigue Analysis, Wiesbaden, Nov. 2000
K. Höschler
Optimization of Model Parameters to Improve Crack Initiation Prediction of Turbine Disks
ICAF-Konferenz, Melbourne (Australien), Mai 1995