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Technical Report on the Selection of a Suitable Flight Test Vehicle for the HYLDA Follow-On Project

Riedel, H. (1996) Technical Report on the Selection of a Suitable Flight Test Vehicle for the HYLDA Follow-On Project. DLR-Interner Bericht. 129-96/23, 71 S.

Full text not available from this repository.

Abstract

The objective of this study is the selection of a suitable flight test vehicle for the HYLDA follow-on project. On the basis of precompetition and the significance of constraints two different procedures offer themselves. If on the one hand the competitive situation with the USA stands in the foreground and if the time constraint is a significant factor, then the choice is for two flight test vehicles. These are in the sequence of operation the A330 for the wing trials at large Reynolds numbers using a wing glove. If on the other hand the time constraint is regarded to be of no significance, the trials of the engine nacelle and the wing glove can be carried out together on an A330, however, with separate demonstrations of the drag reduction achieved by the hybrid laminar flow control for the engine nacelle and the wing glove, respectively.

Item URL in elib:https://elib.dlr.de/36433/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Technical Report on the Selection of a Suitable Flight Test Vehicle for the HYLDA Follow-On Project
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Riedel, H.UNSPECIFIEDUNSPECIFIED
Date:1996
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:71
Status:Published
Keywords:HYLDA Follow-On Project, Flight Testing, Hybrid Laminar Flow Control, Engine Nacelle, Wings, Civil Transport Aircraft
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 (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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