Analyses and Assessment of the Aerodynamic Behavior of Tests with High Swept Aircraft in DNW Wind Tunnels

Schütte, Andreas (2009) Analyses and Assessment of the Aerodynamic Behavior of Tests with High Swept Aircraft in DNW Wind Tunnels. EWA - Demo-Workshop “Dynamic Wind Tunnel Testing”, 28.-30. April 2009, Göttingen, Deutschland.

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Document Type:

Conference or Workshop Item (Speech)

Title:

Analyses and Assessment of the Aerodynamic Behavior of Tests with High Swept Aircraft in DNW Wind Tunnels

Authors:

Authors	Institution or Email of Authors
Schütte, Andreas	DLR-AS-TF

Date:

28 April 2009

Keywords:

delta wing, fighter aircraft, dynamic testsing, MPM, DNW, vortical flow, vortex

Event Title:

EWA - Demo-Workshop “Dynamic Wind Tunnel Testing”

Event Location:

Göttingen, Deutschland

Event Type:

international Conference, Workshop

Event Dates:

28.-30. April 2009

Organizer:

EWA - European Wind Tunnel Association

HGF - Research field:

no assignement

HGF - Program:

Aeronautics

HGF - Program Themes:

L RR - Rotorcraft Research

DLR - Research area:

Aeronautics

DLR - Program:

L RR - Rotorcraft Research

DLR - Research theme (Project):

L - The Specialised Military Rotorcraft (old)

Location:

Braunschweig

Institutes and Institutions:

Institute of Aerodynamics and Flow Technology

Deposited By:

Andreas Schütte

Deposited On:

15 Dec 2009 13:33

Last Modified:

15 Jan 2010 02:20

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