ALVAST Half-Model Wind Tunnel Investigations and Comparison with Full-Span Model Results

Puffert-Meißner, W. (1996) ALVAST Half-Model Wind Tunnel Investigations and Comparison with Full-Span Model Results. DLR-Interner Bericht. 129-96/20. 70 S.

Full text not available from this repository.

Abstract

The ALVAST half-model was investigated in a cruise configuration and a take-off configuration with and without Through-Flow Nacelle in the DNW-NWB Low-Speed Wind Tunnel Braunschweig at Mach numbers of 0.14, 0.18 and 0.22 in order to evaluate the half-model test technique in this wind tunnel. The model geometry and the model mounting in the test section are described. Results of the force and pressure distribution measurements are presented in comparison with full-span model results from DNW-tests and differences are analyzed and discussed.

Item URL in elib:

https://elib.dlr.de/36532/

Document Type:

Monograph (DLR-Interner Bericht)

Additional Information:

LIDO-Berichtsjahr=1996,

Title:

ALVAST Half-Model Wind Tunnel Investigations and Comparison with Full-Span Model Results

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Puffert-Meißner, W.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

1996

Open Access:

Number of Pages:

Status:

Published

Keywords:

Wind Tunnel Tests, Low Speed, Half-Span Model, Full-Span Model, 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

Repository Staff Only: item control page