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Numerical Simulation of the Free Pitch Oscillation for a Re-entry Vehicle in Transonic Wind Tunnel Flow

Reimann, Bodo (2015) Numerical Simulation of the Free Pitch Oscillation for a Re-entry Vehicle in Transonic Wind Tunnel Flow. 8th European Symposium on Aerothermodynamics for Space Vehicles, 2015-03-02 - 2015-03-06, Lissabon, Portugal.

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Item URL in elib:https://elib.dlr.de/98754/
Document Type:Conference or Workshop Item (Speech)
Title:Numerical Simulation of the Free Pitch Oscillation for a Re-entry Vehicle in Transonic Wind Tunnel Flow
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Reimann, BodoUNSPECIFIEDhttps://orcid.org/0000-0001-7765-7295UNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:dynamic stability, pitch damping, derivatives, free oscillation technique, flight mechanics coupling, sting effects, CFD, TAU-code, chimera technique
Event Title:8th European Symposium on Aerothermodynamics for Space Vehicles
Event Location:Lissabon, Portugal
Event Type:international Conference
Event Start Date:2 March 2015
Event End Date:6 March 2015
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Reimann, Bodo
Deposited On:20 Oct 2015 13:53
Last Modified:24 Apr 2024 20:04

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