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Virtual Aircraft Technology Integration Platform: From Virtual Flight Testing towards Simulation-based Certification

Ritter, Markus Raimund and Handojo, Vega and Krüger, Wolf R. and Roeser, Mathias Stefan and Mönnich, Wulf and Kirmse, Tania and Reimer, Lars and Heinrich, Ralf and Geisbauer, Sven and Görtz, Stefan (2021) Virtual Aircraft Technology Integration Platform: From Virtual Flight Testing towards Simulation-based Certification. In: AIAA Scitech 2021 Forum. AIAA SciTech 2021 Forum, 2021-01-11 - 2021-01-21, Virtuelle Konferenz. ISBN 978-162410609-5.

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Abstract

The development, testing and production of new aircraft are associated with considerable temporal and financial risks due to the product and manufacturing complexity. In order to accelerate the introduction of innovative technologies for more economical, more environmentally friendly and safer air vehicles and to better control the technological risks involved, DLR's guiding concept The Virtual Product aims at virtualizing the design, development and manufacturing processes, including the definition of an appropriate validation strategy. The availability of high fidelity simulation tools with the capability to model multidisciplinary phenomena is a decisive part in that context. High demands are put on the numerical methods and solvers as the tools must provide reliable results in a robust manner for the entire flight envelope where nonlinearities are prominent in most of the disciplines. A key technology is the ability to enable Virtual Flight Testing based on high-fidelity simulation tools. The progress made at the German Aerospace Center (DLR) in the recent past regarding the development of methods and tools to perform virtual flight tests is presented in two papers. The first paper (Virtual Aircraft Technology Integration Platform: Ingredients for Multidisciplinary Simulation System and Virtual Flight Testing) gives an overview of the development of components required for virtual flight testing. The present paper outlines the methods, the framework, and the simulation models for particular applications, the virtual system identification flights of a medium size jet transport. Aerodynamics, structural dynamics, flight mechanics and propulsion are considered for the massively-parallel, time-domain simulations.

Item URL in elib:https://elib.dlr.de/140808/
Document Type:Conference or Workshop Item (Speech)
Title:Virtual Aircraft Technology Integration Platform: From Virtual Flight Testing towards Simulation-based Certification
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Ritter, Markus RaimundUNSPECIFIEDhttps://orcid.org/0000-0003-3828-0397UNSPECIFIED
Handojo, VegaUNSPECIFIEDhttps://orcid.org/0000-0001-6030-2383UNSPECIFIED
Krüger, Wolf R.UNSPECIFIEDhttps://orcid.org/0000-0002-7949-1169UNSPECIFIED
Roeser, Mathias StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Mönnich, WulfUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Kirmse, TaniaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Reimer, LarsUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Heinrich, RalfUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Geisbauer, SvenUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Görtz, StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:15 January 2021
Journal or Publication Title:AIAA Scitech 2021 Forum
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
ISBN:978-162410609-5
Status:Published
Keywords:virtual flight testing, numerical flight dynamics, loads, CFD, aeroelasticity, multidisciplinary analysis
Event Title:AIAA SciTech 2021 Forum
Event Location:Virtuelle Konferenz
Event Type:international Conference
Event Start Date:11 January 2021
Event End Date:21 January 2021
Organizer:AIAA - American Institute of Aeronautics and Astronautics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Aircraft and  Validation
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Institute of Flight Systems > Flight Dynamics and Simulation
Institute for Aerodynamics and Flow Technology > CASE, BS
Institute for Aerodynamics and Flow Technology > Experimental Methods, GO
Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Ritter, Markus Raimund
Deposited On:09 Feb 2021 16:42
Last Modified:24 Apr 2024 20:41

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