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

Status of Hot Film Analysis of A 320 Laminar Fin Turbulent Reference Flight Test TFT

Hoehler, G. and Kreplin, G. and Baumgarten, D. (1996) Status of Hot Film Analysis of A 320 Laminar Fin Turbulent Reference Flight Test TFT. DLR-Interner Bericht. 223-96 C 25, 26 S.

Full text not available from this repository.

Abstract

The surface hot fil technique was successfully applied to the investigation of attachment line transition on the A 320 fin in the Turbulent Reference Flight Test (TFT). The principal functioning of the Gaster bump design was demonstrated for flight altitudes from 16000 ft to 39000 ft and Mach numbers up to Ma &#61 0.78.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Status of Hot Film Analysis of A 320 Laminar Fin Turbulent Reference Flight Test TFT
Authors:
AuthorsInstitution or Email of Authors
Hoehler, G.UNSPECIFIED
Kreplin, G.UNSPECIFIED
Baumgarten, D.UNSPECIFIED
Date:1996
Number of Pages:26
Status:Published
Keywords:Surface Hot Film Technique, Attachment Line Transition, A 320 Laminar Fin, Gaster Bump
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:08

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.