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Conference Papers & Publications
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- About PACE
- Conference Papers & Publications
Supporting Innovation Through Research
Through our unique products, such as Pacelab APD & SysArc, PACE Aerospace & IT has supported universities, students and research organizations for years, contributing unique, original research to advancing the boundaries of the aerospace engineering sciences.
The list below collects publications produced by our staff for scientific and commercial forums, results from collaborations with universities or studies involving the application of one of our products for preliminary aircraft design.
Direct Coupling of Parallel Hybrid Propulsive System and Vehicle-Level Integrated Mission Performance Aircraft Sizing Models
Joksimović, A., Lourenco-Feio, A., Occhipinti, A., and Domínguez Sanchez, J.
2024 More Electric Aircraft
7-8 February 2024, Toulouse, France
https://conference-mea.org/
Urban Air Vehicle Mission Sizing and Performance Estimation Using Pacelab APD
Occhipinti, A., Joksimovic, A., and Emeneth, M.2023 AIAA SciTech Forum
23–27 January 2023, National Harbor (MD), USA
A Method for the Conceptual Design of Hybrid Electric Aircraft
Zamboni, J., Vos, R., Emeneth, M., and Schneegans, A.
56th AIAA Aerospace Sciences Meeting (AIAA SciTech Forum)
January 7-11, 2019, San Diego (CA), USA
Development and Application of WASPE for Conceptual Design of HEDiP Aircraft
Ganesh, R.V., Raj, P., Choi, S. and Emeneth, M.
Royal Aeronautical Society 2018 Applied Aerodynamics Conference
The Future of Aerodynamics – Research, Development, Simulation and Applications
July 24-26, 2018, Bristol, UK
Sizing, Integration and Performance Evaluation of Hybrid Electric Propulsion Subsystem Architectures
Cinar, G., Mavris, D.N., Emeneth, M., Schneegans, A., Riediger, C., Fefermann, Y., Isikveren, A. (2017)
55th AIAA Aerospace Sciences Meeting (AIAA SciTech Forum)
January 9-13, 2017, Grapevine (TX), USA
Development of Parametric Power Generation and Distribution Subsystem Models at Conceptual Aircraft Design Stage.
Cinar, G., Mavris, D.N., Emeneth, M., Schneegans, A., Fefermann, Y. (2017)
55th AIAA Aerospace Sciences Meeting (AIAA SciTech Forum)
January 9-13, 2017, Grapevine (TX), USA
A Methodology for Sizing and Analysis of Electric Propulsion Subsystems for Unmanned Aerial Vehicles
Cinar, G., Emeneth, M., and Mavris, D.N. (2016)
54th AIAA Aerospace Sciences Meeting (AIAA SciTech Forum)
January 4-8, 2016, San Diego (CA), USA
A Physics-Based Methodology for Cantilever and Strut-Braced Wing Weight Estimation
Locatelli, D., Riggins, B., Kapania, R., Schetz, J., and Poquet, T. (2016)
54th AIAA Aerospace Sciences Meeting (AIAA SciTech Forum)
January 4-8, 2016, San Diego (CA), USA
An integrated approach to vehicle and subsystem sizing and analysis for novel subsystem architectures
Chakraborty, I., Mavris, D.N., Emeneth, M., and Schneegans, A. (2015)
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.
Published online July 20, 2015, DOI: 10.1177/0954410015594399
Development of a Multi-Disciplinary Optimization Framework for Nonconventional Aircraft Configurations in PACELAB APD
Riggins, B., Locatelli, D., Schetz, J., Kapania, R. et al. (2015)
SAE AeroTech Congress & Exhibition
September 22-24, 2015, Seattle (WA), USA
A Methodology for Vehicle and Mission Level Comparison of More Electric Aircraft Subsystem Solutions – Application to the Flight Control Actuation System
Chakraborty, I., Mavris, D.N., Emeneth, M., and Schneegans, A. (2014)
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.
Published online July 28, 2014, DOI: 10.1177/0954410014544303
A Requirements-driven Methodology for Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase
Chakraborty, I., Trawick, D., Mavris, D.N., Emeneth, M., and Schneegans, A. (2014)
14th AIAA Aviation Technology, Integration, and Operations Conference
June 16-20, 2014, Atlanta (GA), USA
AIAA 2015 Best Paper Award – Left to right: Mathias Emeneth (PACE), Imon Chakraborty and Prof. Dimitri N. Mavris (ASDL)
Aircraft Conceptual Design: Tools Evaluation
Locatelli, D., Riggins, B., Schetz, J.A., Kapania, R.K., Robic, B., Leenaert, B., and Poquet, T. (2014)
14th AIAA Aviation Technology, Integration, and Operations Conference
June 16-20, 2014, Atlanta (FL), USA
A System and Mission Level Analysis of Electrically Actuated Flight Control Surfaces using Pacelab SysArc
Chakraborty, I., Mavris, D.N., Emeneth, M., and Schneegans, A. (2014)
AIAA Science and Technology Forum and Exposition (SciTech)
Jan 13-17, 2014, National Harbor (MD), USA
Robust Aircraft Subsystem Conceptual Architecting
Jackson, D.W. (2013)
Ph.D. Georgia Institute of Technology
Optimisation Robuste des Aéronefs et des Groups Turboréacteurs
Couturier, P. (2012)
M.Sc. École polytechnique de Montréal
Parametric Control Surface Modeling During Early Design Stages in Pacelab Suite
Emeneth, M., Garmendia, D., Mavris, D. (2012).
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
January 09-12, 2012, Nashville (TN), USA
Advanced Methods for Propulsion System Integration in Aircraft Conceptual Design
Seitz, A. (2012)
Ph.D. University of Munich
Investigating Systems Architectures at the Aircraft Level – Towards a Holistic Framework for the Aircraft Systems Design Process
Schneegans, A. (2012)
Deutscher Luft- und Raumfahrtkongress
September 10-12, 2012, Berlin, Germany.
Knowledge-Based Preliminary Design of Aero-Engine Gas-Generators
Bretschneider, S. (2011)
Ph.D. University of Stuttgart
Systems Architecture Design – A Software Development for the JTI Clean Sky Green Regional Aircraft Program
Schneegans, A. (2011)
11th AIAA Aviation Technology, Integration, and Operations Conference
September 20-22, 2011, Virginia Beach (VA), USA
The All-Electric Regional Aircraft – A New Design Methodology for Vehicle-Level Systems Architecture Design
Schneegans, A. (2011)
58th Canadian Aeronautics and Space Institute (CASI) Aeronautics Conference - AERO 2011
April 26-28, 2011, Montreal (QC), Canada
A Modeling Methodology and Environment for Integrated Trim Analysis for a Reusable Booster System
Robertson, B., Crowley, D., Garmendia, D., Douglass, R., Mavris, D., and Hellman, B. (2011)
49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
January 4-7, 2011, Orlando (FL), USA
Integrierte Produkt- und Prozessmodellierung. Unterstützung der Systementwicklung für eine Avionik-Plattform (Integrated product and process modelling. Support of system development for avionics)
Girod, M., Schramm, A., Schultz, R., Wintrich, N. (2011)
Zeitschrift für wirtschaftlichen Fabrikbetrieb. ZWF 106 (6). pp.454-457
Comparison of Powered-Lift Turbofan Aircraft with Conventional Turboprop Aircraft for ESTOL Application
Gologan, C., Schmitt, D. (2010)
27th International Congress of Aeronautical Sciences
September 19-24, 2010, Nice, France
New Design Methodology for the Development and Optimization of Payload and System Architectures for Unmanned Aircraft Systems
Ehlermann, F. (2010)
4th International Conference UAV World
November 3-4, 2010, Frankfurt/Main, Germany
Formulation and Implementation of a Methodology for Aircraft Subsystem Architecture Selection
Zaidi, T. (2009)
TEOS III Forum at the 13th European Conference on Power Electronics and Applications
September 8-10, 2009, Barcelona, Spain
Applying KBE Technologies to the Early Phases of Multidisciplinary Product Design
Schneegans, A. and Ehlermann, F. (2007)
In: Frank-Lothar Krause, ed. 2007. The Future of Product Development. Proceedings of the 17th CIRP Design Conference. Berlin: Springer. pp. 587-596