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Validation of CFD Airdrop Simulations in the Vortical Wake of an Aircraft with Open Ramp

Geisbauer, Sven and Schmidt, Hauke (2016) Validation of CFD Airdrop Simulations in the Vortical Wake of an Aircraft with Open Ramp. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer Verlag. pp. 29-38. ISBN 978-3-319-27278-8. ISSN 1612-2909

Full text not available from this repository.

Official URL: http://www.springer.com/de/book/9783319272788

Abstract

During the first few seconds of an airdrop the supplies heavily interact with the wake of the military transport aircraft. Due to the particular shape of their rear fuselage and the voluminous landing gear fairings the flow field behind the aircraft is highly vortical. Flying in airdrop configuration even aggravates the situation. To comprehensively analyze and evaluate the airdrop capabilities of military transport aircraft DLR has developed a simulation approach, coupling the DLR TAU code with the multibody simulation tool SIMPACK. This Approach enables DLR to compute the trajectories of airdropped supplies under full consideration of flow interaction effects. For various cargo and cargo-parachute configurations DLR successfully demonstrated that this approach is well-suited to accurately compute an airdrop sequence. The results of two of these configurations are presented in this paper.

Item URL in elib:https://elib.dlr.de/105564/
Document Type:Contribution to a Collection
Title:Validation of CFD Airdrop Simulations in the Vortical Wake of an Aircraft with Open Ramp
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Geisbauer, Svensven.geisbauer (at) dlr.deUNSPECIFIED
Schmidt, Haukehauke.schmidt (at) dlr.deUNSPECIFIED
Date:2016
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics X
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:132
DOI :10.1007/978-3-319-27279-5_3
Page Range:pp. 29-38
Editors:
EditorsEmail
Dillmann, AndreasDLR Göttingen
Heller, GerdAirbus Bremen
Krämer, EwaldUni Stuttgart
Wagner, ClausDLR Göttingen
Breitsamter, ChristianTU München
Publisher:Springer Verlag
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-319-27278-8
Status:Published
Keywords:Airdrop, transport aircraft, simulation, validation, CFD, multibody, uRANS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Military Technologies
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Seyfried, Beate
Deposited On:10 Aug 2016 11:48
Last Modified:10 Aug 2016 11:48

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