Scientific publications

Contributions to scientific journals:

Kazula, S. und K. 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.

Kazula, S. und K. Höschler. A systems engineering approach to variable intakes for civil aviation. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019. ISSN 0954-4100. doi:10.1177/0954410019836903.

Kazula, S. und K. 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.

Kazula, S., M. Wöllner und K. 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.

Contributions to scientific conferences:

Kazula, S. und K. Höschler. A Systems Engineering Approach to Variable Intakes for Civil Aviation. Proceedings of the 7th European Conference for Aeronautics and Space Sciences (Eucass), Milan, Italy, 2017. doi:10.13009/EUCASS2017-20.

Kazula, S., D. Grasselt, M. Mischke und K. Höschler. Preliminary safety assessment of circular variable nacelle inlet concepts for aero engines in civil aviation. In: S. Haugen, A. Barros, C. van Gulijk, T. Kongsvik und J.E. Vinnem, Hg. Safety and reliability - safe societies in a changing world. Proceedings of the 28th International European Safety and Reliability Conference (ESREL 2018), Trondheim, Norway, 17-21 June 2018. Boca Raton: CRC Press, Taylor et Francis Group, 2018, S. 2459-2467. ISBN 9781351174664. doi:10.1201/9781351174664-309.

Kazula, S., D. Grasselt und K. Höschler. Common Cause Analysis of Circular Variable Nacelle Inlet Concepts for Aero Engines in Civil Aviation. In: J.F. Silva Gomes und S.A. Meguid, Hg. IRF2018. Proceedings of the 6th International Conference on Integrity-Reliability-Failure: (Lisbon/Portugal, 22-26 July 2018). Porto: FEUP-INEGI, 2018. ISBN 978-989-20-8313-1.

Kazula, S. und K. Höschler. Ice detection and protection systems for circular variable nacelle inlet concepts. Proceedings of the Deutscher Luft- und Raumfahrtkongress 2018, Friedrichshafen, Germany, 2018. doi:10.25967/480129.

Kazula, S., B. Rich, K. Höschler und R. Woll. Awakening the Interest of High School Pupils in Science, Technology, Engineering and Mathematics Studies and Careers through Scientific Projects. In: 2018 IEEE International Conference on Teaching, Assessment, and Learning for Engineering (TALE): IEEE, 2018, S. 259-265. ISBN 978-1-5386-6522-0. doi:10.1109/TALE.2018.8615418.

Kazula, S., M. Wöllner, D. Grasselt und K. Höschler. Ideal Geometries and Potential Benefit of Variable Pitot Inlets for Subsonic and Supersonic Business Aviation. Proceedings of the 8th European Conference for Aeronautics and Space Sciences (Eucass), Madrid, Spain, 2019. doi:10.13009/EUCASS2019-314.

Kazula, S., M. Mischke, P. König und K. Höschler. Evaluation of Variable Pitot Inlet Concepts for Transonic and Supersonic Civil Aviation. 9th EASN International Conference on “Innovation in Aviation & Space", MATEC Web of Conferences, 2019, 304(12), 2016. doi:10.1051/matecconf/201930402016.

Kazula, S., M. Wöllner, D. Grasselt und K. Höschler. Parametric Design Study on Aerodynamic Characteristics of Variable Pitot Inlets for Transonic and Supersonic Civil Aviation. 9th EASN International Conference on “Innovation in Aviation & Space", MATEC Web of Conferences, 2019, 304(12), 2017. doi:10.1051/matecconf/201930402017.

Kazula, S., M. Wöllner, D. Grasselt und K. Höschler. Parametric design and aerodynamic analysis of circular variable aero engine inlets for transonic and supersonic civil aviation. Proc. of the 24th International Symposium on Air Breathing Engines, 2019, (ISABE-2019-24018) [Zugriff am: 5. Juni 2020]. Verfügbar unter: drive.google.com/drive/folders/1PZaMaLOLsybB3KFLmvP8hwM_lwmk3e4B

Kazula, S. und K. Höschler. A Variable Pitot Inlet Concept for Supersonic Aviation. Proceedings of Global Power and Propulsion Society GPPS Chania20, 2020, im Druck.

Kazula, S. und K. Höschler. Review of Variable Leading Edge Patents for Aircraft Wings and Engine Inlets and Their Relevance for Variable Pitot Inlets in Future Supersonic Transport. Proceedings of the Deutscher Luft- und Raumfahrtkongress 2020, 2020, in Vorbereitung.

Co-author contributions:

Grasselt, D., K. Höschler und S. Kazula. A Design Approach for a Coupled Actuator System for Variable Nozzles and Thrust Reverser of Aero Engines. Proc. of the 23rd International Symposium on Air Breathing Engines, 2017.

Rich, B.M., J. Worlitz, C. Goldmann, M. Schulze, S. Kazula und R. Woll. Preparing STEM Students for Leading Positions through Supervising Younger Students. In: 2018 IEEE International Conference on Teaching, Assessment, and Learning for Engineering (TALE): IEEE, 2018, S. 835-839. ISBN 978-1-5386-6522-0. doi:10.1109/TALE.2018.8615359.

Mischke, M., S. Kazula und K. 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, 2019.

Mischke, M., S. Kazula und K. Hoeschler. Preliminary safety Assessment on System Design Level for Broadband Acoustic Liner Concepts for Aviation. MATEC Web of Conferences, 2019, 304, 4010. doi:10.1051/matecconf/201930404010.

König, P., M. Mischke, S. Kazula und K. Höschler. Concept Development and Evaluation for a Broadband Noise Absorbing Acoustic Liner Concept for Aviation. Proc. of the 24th International Symposium on Air Breathing Engines, 2019.

Konstantinidis, A., K. Höschler und S. Kazula. Creating Desired Decoupled Component Properties by a Structural Optimisation Approach based on CAD Geometries. Proc. of NAFEMS European Conference: Simulation-Based Optimisation, 2019.

Other publications:

David Grasselt, Prof. Dr.-Ing. 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, Prof. Dr.-Ing. 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, Prof. Dr.-Ing. 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, Prof. Dr.-Ing. Klaus Höschler, "Aerodynamic Assessment of Nozzle Area Variation by Core Fairing Modulation" Deutscher Luft- und Raumfahrtkongress (DLRK), 22.-24. September 2015, Rostock

Chetan Kumar Sain, Prof. Dr.-Ing. 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, Prof. Dr.-Ing. 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, Prof. Dr.-Ing. 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, Prof. Dr.-Ing. 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.