PACE
Research
Research
PACE
Research
Research
Papers &
Publications
Publications
SUPPORTING INNOVATION.
PACE regularly publishes research on key R&D topics in our industry. Below is a collection of our team’s publications, including collaborative projects with universities and studies using our product in preliminary aircraft design DESMO, formerly known as Pacelab APD & SysArc.
Integrated Preliminary Sizing Environment for Hydrogen-Powered Drones
Feio, A., Joksimović, A.,Gavrilović N. 2025 AIAA SciTech Forum 6-10 January 2025, Orlando (FL), USA
An Economical Viability Exploration of Three Sustainable Regional Aircraft Concepts in Sweden
Espinosa-Juárez, E., Jouannet, C., Amadori, K. 2025 AIAA SciTech Forum 6-10 January 2025, Orlando (FL), USA
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
Formulation and Implementation of a Methodology for Aircraft Subsystem Architecture Selection
Turab Zaidi 2008 - 2009 Grand Challenge Team, Aerospace Systems Design Laboratory, Georgia Institute of Technology, Atlanta, GA, USA
Sizing, Integration and Performance Evaluation of Hybrid Electric Propulsion Subsystem Architectures
Gokcin Cinar, Dimitri N. Mavris, Mathias Emeneth, Alexander Schneegans, Carsten Riediger, Yann Fefermann and Askin Isikveren. AIAA 2017-1183 Session: Electric Aircraft Design. Published Online:5 Jan 2017
Development of Parametric Power Generation and Distribution Subsystem Models at the Conceptual Aircraft Design Stage
Gokcin Cinar, Dimitri N. Mavris, Mathias Emeneth, Alexander Schneegans and Yann FefermannAIAA 2017-1182Session: Electric Aircraft DesignPublished Online:5 Jan 2017
Comparison Of Powered-Lift Turbofan Aircraft With Conventional Turboprop Aircraft For Estol Application
Gokcin Cinar, Dimitri N. Mavris, Mathias Emeneth, Alexander Schneegans and Yann FefermannAIAA 2017-1182Session: Electric Aircraft DesignPublished Online:5 Jan 2017
Advanced Methodsfor Propulsion System Integrationin Aircraft Conceptual Design
Arne Seitz - TECHNISCHE UNIVERSITAT MUNCHEN "Institut fur Luft- und Raumfahrt" 2011
Optimisation Robuste Des Aeronefs Et Des Groupes Turboreacteurs
PHILIPPE COUTURIER Departement de Genie Mecanique Ecole Polytechnique de Montreal - 2012
Investigating Systems Architectures At The Aircraft Level– Towards A Holistic Framework For Theaircraft Systems Design Process
A. Schneegans,PACE Aerospace Engineering and Information Technology GmbH,Rotherstr. 20, 10245 Berlin, Germany
Development and application of WASPE forconceptual design of HEDiP aircraft
R. V. Ganesh - P. Raj S. Choi - Kevin T. Crofton - Department of Aerospace and Ocean Engineering Virginia Polytechnic Institute and State University Blacksburg, Virginia, USA - M. Emeneth PACE America Inc.USA