elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Role of HPC in Aircraft Design

Kroll, Norbert (2013) Role of HPC in Aircraft Design. PRACE Industrial Seminar, 15.-16. April 2013, Bad Boll, Deutschland.

Full text not available from this repository.

Abstract

In recent years, the aeronautical industriy has established numerical flow simulations as a key element in the aerodynamic design process, complementing wind tunnel and flight tests. The continuous development of physical models and numerical methods and the availability of increasingly powerful computers suggest using numerical simulations to a much greater extent than before, radically chaning the way aircraft will be designed in the future. The vision of an aircraft performing its "maiden flight" in a virtual computer environment is the focus of future research in numerical simulation in aeronautics. One of the primary objectives is the development and deployment of a flexible, parallel software platform for multidisciplinary analysis and optimization of aircraft based on high-fidelity numerical methods for each discipline involved. This platform should break up the predominantly sequential approach currently used in detail design and should make available the full potential of multidisciplinary design. The multidisciplinary simulation platform should also make it possible to efficiently and reliably perform manoeuvre simulations throughout the entire flight envelope, and thus permit the determination of aerodynamic and aeroelastic data for evaluating the handling qualities based on high-fidelity numerical methods. The very complex, multidisciplinary simulations and the challenges in terms of physical modeling across the flight envelope require enormous HPC resources and further developments and improvements of flow solvers (CFD). Given the technology development of high-performance computers, most CFD solvers used today have reached the limit of scalability when it comes to parallelization. Therefore, design and implementation of a next-generation flow solver taking advantage of the upcoming computer architecture is to be regarded as a future investment of aeronautical research and industry. The presentation will describe some of the target applications for virtual analysis and testing in aircraft design. Based on the current status of the CFD methods the major challenges and requirements for further development will be derived.

Item URL in elib:https://elib.dlr.de/86407/
Document Type:Conference or Workshop Item (Speech)
Title:Role of HPC in Aircraft Design
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kroll, Norbertnorbert.kroll (at) dlr.deUNSPECIFIED
Date:2013
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Numerical flow simulations, aerodynamic design process, multidisciplinary design, manoeuvre simulations, high-performance computers
Event Title:PRACE Industrial Seminar
Event Location:Bad Boll, Deutschland
Event Type:Other
Event Dates:15.-16. April 2013
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation & Validation (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Seyfried, Beate
Deposited On:10 Dec 2013 15:06
Last Modified:08 May 2014 23:19

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.