Slosh dynamics

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Water sloshing in the swimming pool of a cruise ship undergoing pitching motion Slosh in Pool 20150719.jpg
Water sloshing in the swimming pool of a cruise ship undergoing pitching motion

In fluid dynamics, slosh refers to the movement of liquid inside another object (which is, typically, also undergoing motion).

Contents

Strictly speaking, the liquid must have a free surface to constitute a slosh dynamics problem, where the dynamics of the liquid can interact with the container to alter the system dynamics significantly. [1] Important examples include propellant slosh in spacecraft tanks and rockets (especially upper stages), and the free surface effect (cargo slosh) in ships and trucks transporting liquids (for example oil and gasoline). However, it has become common to refer to liquid motion in a completely filled tank, i.e. without a free surface, as "fuel slosh".[ not verified in body ]

Such motion is characterized by "inertial waves" and can be an important effect in spinning spacecraft dynamics. Extensive mathematical and empirical relationships have been derived to describe liquid slosh. [2] [3] These types of analyses are typically undertaken using computational fluid dynamics and finite element methods to solve the fluid-structure interaction problem, especially if the solid container is flexible. Relevant fluid dynamics non-dimensional parameters include the Bond number, the Weber number, and the Reynolds number.

Water sloshing in a glass cup

Slosh is an important effect for spacecraft, [4] ships, [3] some land vehicles and some aircraft. Slosh was a factor in the Falcon 1 second test flight anomaly, and has been implicated in various other spacecraft anomalies, including a near-disaster [5] with the Near Earth Asteroid Rendezvous (NEAR Shoemaker) satellite.

Spacecraft effects

Liquid slosh in microgravity [6] [7] is relevant to spacecraft, most commonly Earth-orbiting satellites, and must take account of liquid surface tension which can alter the shape (and thus the eigenvalues) of the liquid slug. Typically, a large fraction of the mass of a satellite is liquid propellant at/near Beginning of Life (BOL), and slosh can adversely affect satellite performance in a number of ways. For example, propellant slosh can introduce uncertainty in spacecraft attitude (pointing) which is often called jitter. Similar phenomena can cause pogo oscillation and can result in structural failure of a space vehicle.

Another example is problematic interaction with the spacecraft's Attitude Control System (ACS), especially for spinning satellites [8] which can suffer resonance between slosh and nutation, or adverse changes to the rotational inertia. Because of these types of risk, in the 1960s the National Aeronautics and Space Administration (NASA) extensively studied [9] liquid slosh in spacecraft tanks, and in the 1990s NASA undertook the Middeck 0-Gravity Dynamics Experiment [10] on the Space Shuttle. The European Space Agency has advanced these investigations [11] [12] [13] [14] with the launch of SLOSHSAT. Most spinning spacecraft since 1980 have been tested at the Applied Dynamics Laboratories drop tower using sub-scale models. [15] Extensive contributions have also been made [16] by the Southwest Research Institute, but research is widespread [17] in academia and industry.

Research is continuing into slosh effects on in-space propellant depots. In October 2009, the Air Force and United Launch Alliance (ULA) performed an experimental on-orbit demonstration on a modified Centaur upper stage on the DMSP-18 satellite launch in order to improve "understanding of propellant settling and slosh", "The light weight of DMSP-18 allowed 12,000 pounds (5,400 kg) of remaining LO2 and LH2 propellant, 28% of Centaur’s capacity", for the on-orbit tests. The post-spacecraft mission extension ran 2.4 hours before the planned deorbit burn was executed. [18]

NASA's Launch Services Program is working on two on-going slosh fluid dynamics experiments with partners: CRYOTE and SPHERES-Slosh. [19] ULA has additional small-scale demonstrations of cryogenic fluid management are planned with project CRYOTE in 2012–2014 [20] leading to a ULA large-scale cryo-sat propellant depot test under the NASA flagship technology demonstrations program in 2015. [20] SPHERES-Slosh with Florida Institute of Technology and Massachusetts Institute of Technology will examine how liquids move around inside containers in microgravity with the SPHERES Testbed on the International Space Station.

Sloshing in road tank vehicles

Liquid sloshing strongly influences the directional dynamics and safety performance of highway tank vehicles in a highly adverse manner. [21] Hydrodynamic forces and moments arising from liquid cargo oscillations in the tank under steering and/or braking maneuvers reduce the stability limit and controllability of partially-filled tank vehicles. [22] [23] [24] Anti-slosh devices such as baffles are widely used in order to limit the adverse liquid slosh effect on directional performance and stability of the tank vehicles. [25] Since most of the time, tankers are carrying dangerous liquid contents such as ammonia, gasoline and fuel oils, stability of partially-filled liquid cargo vehicles is very important. Optimizations and sloshing reduction techniques in fuel tanks such as elliptical tank, rectangular, modified oval and generic tank shape have been performed in different filling levels using numerical, analytical and analogical analyses. Most of these studies concentrate on effects of baffles on sloshing while the influence of cross-section is completely ignored. [26]

The Bloodhound LSR 1,000 mph project car utilizes a liquid-fuelled rocket that requires a specially-baffled oxidizer tank to prevent directional instability, rocket thrust variations and even oxidizer tank damage. [27]

Practical effects

Sloshing or shifting cargo, water ballast, or other liquid (e.g., from leaks or fire fighting) can cause disastrous capsizing in ships due to free surface effect; this can also affect trucks and aircraft.

The effect of slosh is used to limit the bounce of a roller hockey ball. Water slosh can significantly reduce the rebound height of a ball [28] but some amounts of liquid seem to lead to a resonance effect. Many of the balls for roller hockey commonly available contain water to reduce the bounce height.

See also

Related Research Articles

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A monopropellant rocket is a rocket that uses a single chemical as its propellant.

Centaur (rocket stage) Family of rocket stages which can be used as a space tug

The Centaur is a family of rocket propelled upper stages produced by U.S. launch service provider United Launch Alliance, with one main active version and one version under development. The 3.05 m (10.0 ft) diameter Common Centaur/Centaur III flies as the upper stage of the Atlas V launch vehicle, and the 5.4 m (18 ft) diameter Centaur V is being developed as the upper stage of ULA's new Vulcan rocket. Centaur was the first rocket stage to use liquid hydrogen (LH2) and liquid oxygen (LOX) propellants, a high-energy combination that is ideal for upper stages but has significant handling difficulties.

A propellant is a mass that is expelled or expanded in such a way as to create a thrust or other motive force in accordance with Newton's third law of motion, and "propel" a vehicle, projectile, or fluid payload. In vehicles, the engine that expels the propellant is called a reaction engine. Although technically a propellant is the reaction mass used to create thrust, the term "propellant" is often used to describe a substance which is contains both the reaction mass and the fuel that holds the energy used to accelerate the reaction mass. For example, the term "propellant" is often used in chemical rocket design to describe a combined fuel/propellant, although the propellants should not be confused with the fuel that is used by an engine to produce the energy that expels the propellant. Even though the byproducts of substances used as fuel are also often used as a reaction mass to create the thrust, such as with a chemical rocket engine, propellant and fuel are two distinct concepts.

Launch pad Facility from which rockets are launched

A launch pad is an above-ground facility from which a rocket-powered missile or space vehicle is vertically launched. The term launch pad can be used to describe just the central launch platform, or the entire complex. The entire complex will include a launch mount or launch platform to physically support the vehicle, a service structure with umbilicals, and the infrastructure required to provide propellants, cryogenic fluids, electrical power, communications, telemetry, rocket assembly, payload processing, storage facilities for propellants and gases, equipment, access roads, and drainage.

AS-203 Uncrewed flight of the Saturn IB rocket, July 5, 1966

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Orbital propellant depot Cache of propellant that is placed in orbit to allow spacecraft to refuel in space

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Launch Services Program

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SLOSHSAT-FLEVO is a microsatellite launched to investigate the dynamics of fluids in microgravity. FLEVO stands for Facility for Liquid Experimentation and Verification in Orbit. Multiple sensors were used to monitor the behavior of water in an instrumented tank and how sloshing affects the attitude control of launchers and space vehicles.

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A slosh baffle is a device used to dampen the adverse effects of liquid slosh in a tank. Slosh baffles have been implemented in a variety of applications including tanker trucks, and liquid rockets, although any moving tank containing liquid may employ them.

Andrew J. Stofan Engineer

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References

  1. ↑ Moiseyev, N.N. & V.V. Rumyantsev. "Dynamic Stability of Bodies Containing Fluid." Springer-Verlag, 1968.
  2. ↑ Ibrahim, Raouf A. (2005). Liquid Sloshing Dynamics: Theory and Applications. Cambridge University Press. ISBN   978-0521838856.
  3. 1 2 Faltinsen, Odd M.; Timokha, Alexander N. (2009). Sloshing. Cambridge University press. ISBN   978-0521881111.
  4. ↑ Reyhanoglu, M. (23–25 June 2003). Maneuvering control problems for a spacecraft with unactuated fuel slosh dynamics. IEEE Conference on Control Applications. Vol. 1. Istanbul: IEEE. pp. 695–699. doi:10.1109/CCA.2003.1223522.
  5. ↑ Veldman, A. E. P.; Gerrits, J.; Luppes, R.; Helder, J. A.; Vreeburg, J. P. B. (2007). "The numerical simulation of liquid sloshing on board spacecraft". Journal of Computational Physics. 224 (1): 82–99. doi:10.1016/j.jcp.2006.12.020.
  6. ↑ Monti, R. "Physics of Fluids in Microgravity." CRC, 2002.
  7. ↑ Antar, B.N. & V.S. Nuotio-Antar. "Fundamentals of Low Gravity Fluid Dynamics and Heat Transfer." CRC, 1994.
  8. ↑ Hubert, C. "Behavior of Spinning Space Vehicles with Onboard Liquids." NASA GSFC Symposium, 2003.
  9. ↑ Abramson, H.N. "The Dynamic Behavior of Liquids in Moving Containers." NASA SP-106, 1966.
  10. ↑ Crawley, E.F. & M.C. Van Schoor & E.B. Bokhour. "The Middeck 0-Gravity Dynamics Experiment: Summary Report", NASA-CR-4500, Mar 1993.
  11. ↑ Vreeburg, J.P.B. "Measured States of SLOSHSAT FLEVO", IAC-05-C1.2.09, Oct 2005.
  12. ↑ Prins, J.J.M. "SLOSHSAT FLEVO Project, Flight and Lessons Learned", IAC-05-B5.3./B5.5.05, Oct 2005.
  13. ↑ Luppes, R. & J.A. Helder & A.E.P. Veldman. "Liquid Sloshing in Microgravity", IAC-05-A2.2.07, Oct 2005.
  14. ↑ Vreeburg, J. P. B. (2008). "Sloshsat Spacecraft Calibration at Stationary Spin Rates". Journal of Spacecraft and Rockets. 45 (1): 65–75. doi:10.2514/1.30975.
  15. ↑ "Partial List of Spacecraft Tested by ADL". Applied Dynamics Laboratories. Retrieved 30 April 2013.
  16. ↑ "18-Fluid Dynamics in Space Vehicles Brochure". Swri.org. Retrieved 2012-03-09.
  17. ↑ "Slosh Central". Sloshcentral.bbbeard.org. Retrieved 2012-03-09.
  18. ↑ ulalaunch.com Archived 2011-07-17 at the Wayback Machine ; Successful Flight Demonstration Conducted by the Air Force and United Launch Alliance Will Enhance Space Transportation: DMSP-18, United Launch Alliance , October 2009, accessed 2011-01-10.
  19. ↑ nasa.gov
  20. 1 2 spirit.as.utexas.edu Archived 2011-02-06 at the Wayback Machine ; Propellant Depots Made Simple, Bernard Kutter, United Launch Alliance, FISO Colloquium, 2010-11-10, accessed 2011-01-10.
  21. ↑ Kolaei, Amir; Rakheja, Subhash; Richard, Marc J. (2016-01-25). "An efficient methodology for simulating roll dynamics of a tank vehicle coupled with transient fluid slosh". Journal of Vibration and Control. 23 (19): 3216–3232. doi:10.1177/1077546315627565. ISSN   1077-5463.
  22. ↑ Kolaei, Amir; Rakheja, Subhash; Richard, Marc J. (2014-01-06). "Range of applicability of the linear fluid slosh theory for predicting transient lateral slosh and roll stability of tank vehicles". Journal of Sound and Vibration. 333 (1): 263–282. Bibcode:2014JSV...333..263K. doi:10.1016/j.jsv.2013.09.002.
  23. ↑ Kolaei, Amir; Rakheja, Subhash; Richard, Marc J. (2014-07-01). "Effects of tank cross-section on dynamic fluid slosh loads and roll stability of a partly-filled tank truck". European Journal of Mechanics B. 46: 46–58. Bibcode:2014EJMF...46...46K. doi:10.1016/j.euromechflu.2014.01.008.
  24. ↑ Kolaei, Amir; Rakheja, Subhash; Richard, Marc J. (2015-09-01). "Three-dimensional dynamic liquid slosh in partially-filled horizontal tanks subject to simultaneous longitudinal and lateral excitations". European Journal of Mechanics B. 53: 251–263. Bibcode:2015EJMF...53..251K. doi:10.1016/j.euromechflu.2015.06.001.
  25. ↑ Kolaei, Amir; Rakheja, Subhash; Richard, Marc J. (2015-01-31). "A coupled multimodal and boundary-element method for analysis of anti-slosh effectiveness of partial baffles in a partly-filled container". Computers & Fluids. 107: 43–58. doi:10.1016/j.compfluid.2014.10.013.
  26. ↑ Talebitooti, R.; shojaeefard, M.H.; Yarmohammadisatri, Sadegh (2015). "Shape design optimization of cylindrical tank using b-spline curves". Computer & Fluids. 109: 100–112. doi:10.1016/j.compfluid.2014.12.004.
  27. ↑ "29, the Importance of Slosh and Slam". 2012-06-29.
  28. ↑ Sport ball for roller hockey; U.S. Patent 5516098; May 14, 1996; Jeffrey Aiello.

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