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Aerodynamic Aspects of Engine-Aircraft Integration of Transport Aircraft

Hoheisel, H. (1997) Aerodynamic Aspects of Engine-Aircraft Integration of Transport Aircraft. Aerospace Science and Technology, Vol. 1, pp. 475-487.

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Abstract

The contribution highlights different aspects of engine-airframe integration and summarizes aeras of concern for engine installation such as, engine development trends, turbofan integration with respect to advanced engine concepts, programmes and investigations on propeller integration, application of theoretical methods in particular with respect to viscous effects, engine location, nacelle design and flow aspects as well as jet flows.

Item URL in elib:https://elib.dlr.de/36604/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=1997,
Title:Aerodynamic Aspects of Engine-Aircraft Integration of Transport Aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hoheisel, H.UNSPECIFIEDUNSPECIFIED
Date:1997
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:Vol. 1
Page Range:pp. 475-487
Status:Published
Keywords:Aerodynamics, Numerical Methods, Flow Simulation, Engine Jet Flow
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:06

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