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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:
AuthorsInstitution or Email of Authors
Schütte, AndreasDLR-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:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft
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:12 Dec 2013 20:47

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