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

Wing Design Concepts for Laminar Flow Technology Applications

Schmitt, V. and Horstmann, K.H. (1998) Wing Design Concepts for Laminar Flow Technology Applications. ECCOMAS 98, Athen (gr), 07.-11-09.1998.

Full text not available from this repository.

Abstract

The paper deals with the aerodynamic design of laminar flow wings. The main concepts at present applied which are Natural Laminar Flow (NLF) based on favorable pressure gradients and Hybrid Laminar (HLF) using in addition leading edge suction are presented and discussed. The essential role of a reliable transition prediction in the design process is pointed out. Specific design features of the suction system are also addressed. In addition, some aspects of the off-design problems are raised.

Item URL in elib:https://elib.dlr.de/13207/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Wing Design Concepts for Laminar Flow Technology Applications
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schmitt, V.ONERAUNSPECIFIED
Horstmann, K.H.UNSPECIFIEDUNSPECIFIED
Date:1998
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:transition mechanisms on swept wings, transition prediction, natural laminar flow, hybrid laminar flow, suction system, off-design
Event Title:ECCOMAS 98, Athen (gr), 07.-11-09.1998
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: Grant, Claudia
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:07

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.