Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Jörg Klatte"'
This paper presents recent 1:1 scaled tests results for sloshing, pressurization and evacuation behaviour in membrane tanks used for spacecrafts and satellites. The first 1:1 scale sloshing test setup evaluates fluid reaction forces for axial, latera
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d19f6752f90c0d3fb2ea59b0b6a5d182
https://elib.dlr.de/136020/
https://elib.dlr.de/136020/
Autor:
Lauren M. Sharp, Ryan Jenson, Andrew Wollman, Robert D. Green, Mark M. Weislogel, Jörg Klatte, Peter J. Canfield, Michael Dreyer
Publikováno v:
International Journal of Multiphase Flow. 65:68-81
The ability to separate liquid and gas phases in the absence of a gravitational acceleration has proven a challenge to engineers since the inception of space exploration. Due to our singular experience with terrestrial systems, artificial body forces
Autor:
Jörg Klatte, Jens Gerstmann, Philipp Behruzi, Peter Nöding, Anton Stark, Martin Konopka, Nicolas Darkow
The accurate prediction of the mechanical and thermodynamic behavior of cryogenic liquids in tanks of liquid propelled rocket stages is critical for the design of the tank layout, the pressurization system, and the control algorithm. To analyse the b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1bffed86bfafeeb751b1563a57a2c756
https://elib.dlr.de/105016/
https://elib.dlr.de/105016/
Publikováno v:
Journal of Spacecraft and Rockets. 47:670-679
DOI: 10.2514/1.47343 This paper introduces a video database reduced from the handheld capillary flow contact line experiments completed aboard the International Space Station during expeditions 9–16, August 2004–November 2007. The simple fluid in
Autor:
Michael Dreyer, Mark M. Weislogel, Ryan Jenson, Steven H. Collicott, Jörg Klatte, Yongkang Chen
Publikováno v:
Acta Astronautica. 65:861-869
This paper provides a current overview of the in-flight operations and experimental results of the capillary flow experiment (CFE) performed aboard the International Space Station (ISS) beginning August 2004 to present, with at least 16 operations to
Publikováno v:
Acta Mechanica. 201:269-276
The surface evolver (SE) algorithm is a valued numerical tool for computations of complex equilibrium interfacial phenomena. In this work, an iterative procedure is implemented such that SE can be employed to predict steady-state flows along capillar
Publikováno v:
Journal of Fluid Mechanics. 600:271-289
This paper is concerned with steady and unsteady flow rate limitations in open capillary channels under low-gravity conditions. Capillary channels are widely used in Space technology for liquid transportation and positioning, e.g. in fuel tanks and l
Autor:
C. Marshall, Nasa George, Nicolas Fries, Philipp Behruzi, Diana Gaulke, Adam Butt, Jörg Klatte
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
In November 2014 the development of the propellant tanks for the MPCV ESM (MultiPurpose Crew Vehicle, European Service Module) has passed the Preliminary Design Review (PDR) and is currently approaching the Critical Design Review (CDR). The MPCV is e
Autor:
Peter J. Canfield, Lars Kiewidt, Aleksander Grah, Michael Dreyer, Mark M. Weislogel, W. Blackmore, Jörg Klatte, Ryan Jenson, Y. Chen, P. M. Bronowicki
Publikováno v:
Experiments in fluids 54 (2013) 5
Experiments in fluids, 54(5)
Experiments in fluids, 54(5)
This paper describes the experiments on flow rate limitation in open capillary channel flow that were performed on board the International Space Station in 2011. Free surfaces (gas-liquid interfaces) of open capillary channels balance the pressure di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3bdfc571649845caa6e0800a4a296b54
https://research.wur.nl/en/publications/the-capillary-channel-flow-experiments-on-the-international-space
https://research.wur.nl/en/publications/the-capillary-channel-flow-experiments-on-the-international-space
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In low gravity flight phases without main thrust activations, the liquid tends to wet or migrate along the walls or interior structures within the spacecraft tanks. In many cases a combination of buoyancy effects, e.g. during RCS firing, and capillar