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

Numerical Investigation of the Flow Around a Fuselage/Canard Configuration for a Long Range, Ultra High Capacity Aircraft

Wichmann, G. and Rohardt, C.-H. (1995) Numerical Investigation of the Flow Around a Fuselage/Canard Configuration for a Long Range, Ultra High Capacity Aircraft. DLR-Interner Bericht. 129-95/4, 65 S.

Full text not available from this repository.

Abstract

Within the scope of the development of a long range, ultra high capacity aircraft (UHCA) at Airbus Industrie also the application of a three surface configuration including a front fuselage canard is discussed. Therefore as a contract work for Airbus Industrie at DLR a numerical study concerning the flow around a fuselage/canard configuration has been performed with the aim to prove the aerodynamic feasibility of such a configuration especially in the high subsonic Mach number range. The fuselage geometry and canard planform has been given by Airbus Industrie as well as the geometrical constraints and the aerodynamic conditions. The investigations have been done using the DLR Euler code CEVCATS developed for the analysis of inviscid compressible flow. In the first part of the study the flow field of the front fuselage has been analyzed in detail.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1995,
Title:Numerical Investigation of the Flow Around a Fuselage/Canard Configuration for a Long Range, Ultra High Capacity Aircraft
Authors:
AuthorsInstitution or Email of Authors
Wichmann, G.UNSPECIFIED
Rohardt, C.-H.UNSPECIFIED
Date:1995
Number of Pages:65
Status:Published
Keywords:Three surface aircraft, Ultra High Capacity Aircraft (UHCA), Fuselage/Canard configuration, Transonic flow, Euler analysis
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:05

Repository Staff Only: item control page

Browse
Search
Help & Contact
Informationen
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.