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.

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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.

Item URL in elib:

https://elib.dlr.de/37452/

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:

Authors	Institution or Email of Authors	Author's ORCID iD
Hoehler, G.	UNSPECIFIED	UNSPECIFIED
Kreplin, G.	UNSPECIFIED	UNSPECIFIED
Baumgarten, D.	UNSPECIFIED	UNSPECIFIED

Date:

1996

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Number of Pages:

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:

DLR-Beauftragter, elib

Deposited On:

03 Apr 2006

Last Modified:

27 Apr 2009 10:08

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