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

Comparison of Two Design Codes for Transonic Airfoils.

Hua, J. (1) and Köster, H. (1990) Comparison of Two Design Codes for Transonic Airfoils. DLR-Interner Bericht. 129-90/36, 95 S.

Full text not available from this repository.

Abstract

Within the framework of DLR-CAE cooperation two design codes for transonic airfoils are exchanged. The first method is developed at NPU, Xian, China, and based on the iterative residual correction concept; the second one is a DLR modification of the artificial viscosity method of McFadden. Parameter investigations with both methods have been carried out,several different design examples have been performed. The results are compared and show that both methods are equally capable in designing transonic airfoils.

Item URL in elib:https://elib.dlr.de/35865/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1990,
Title:Comparison of Two Design Codes for Transonic Airfoils.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hua, J. (1)UNSPECIFIEDUNSPECIFIED
Köster, H.UNSPECIFIEDUNSPECIFIED
Date:1990
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:95
Status:Published
Keywords:Design Methods, Airfoil Design
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
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 10:04

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.