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Application of a Coupling of Flight Mechanics and Aerodynamics to predict the SHEFEX I Ascent Phase

Eggers, Thino and Bartolome Calvo, Javier and Wolkow, S. (2013) Application of a Coupling of Flight Mechanics and Aerodynamics to predict the SHEFEX I Ascent Phase. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 121. Springer Verlag. pp. 67-74. doi: 10.1007/978-3-642-35680-3. ISBN 978-3-642-35679-7. ISSN 1612-2909.

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Item URL in elib:https://elib.dlr.de/95721/
Document Type:Contribution to a Collection
Title:Application of a Coupling of Flight Mechanics and Aerodynamics to predict the SHEFEX I Ascent Phase
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Eggers, ThinoUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Bartolome Calvo, JavierUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Wolkow, S.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2013
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics VIII
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:121
DOI:10.1007/978-3-642-35680-3
Page Range:pp. 67-74
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Dillmann, AndreasDLR GöttingenUNSPECIFIEDUNSPECIFIED
Heller, GerdAirbus DeutschlandUNSPECIFIEDUNSPECIFIED
Kreplin, Hans-PeterDLR GöttingenUNSPECIFIEDUNSPECIFIED
Nitsche, WolfgangTU BerlinUNSPECIFIEDUNSPECIFIED
Peltzer, InkenBeechcraft BerlinUNSPECIFIEDUNSPECIFIED
Publisher:Springer Verlag
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-642-35679-7
Status:Published
Keywords:hypersonic aerodynamics, flight mechanics
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 - Konzepte und Entwurf (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Seyfried, Beate
Deposited On:24 Mar 2015 15:56
Last Modified:24 Mar 2015 15:56

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