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Relevant bibliographies by topics / Cryogenic tank

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Academic literature on the topic 'Cryogenic tank'

Author: Grafiati

Published: 18 April 2022

Last updated: 30 July 2025

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Journal articles on the topic "Cryogenic tank"

1

Yang, Fan, Chao Zhang, and Bochao Zhang. "Comparative Study and Analysis of Cryogenic Storage Tanks with Different Storage Energy Media." Journal of Physics: Conference Series 2565, no. 1 (2023): 012028. http://dx.doi.org/10.1088/1742-6596/2565/1/012028.

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Abstract Liquefied natural gas (LNG), ethylene, ethane, propane, and other clean energy are often stored in a cryogenically frozen state on a large scale. As the core equipment of cryogenic energy storage tanks, if different cryogenic energy media are stored, there are certain differences in the design of the storage tanks. Although the design specifications differ little, there is a lack of systematic research. This paper compares the material, process, structure, construction, and commissioning of cryogenic storage tanks such as ethylene, ethane, propane, and LNG storage tanks, and studies t

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2

Singh, Saurabh Kumar, Atul Sharma, and M. D. Atrey. "Heat transfer study on cryogen evaporation in stationary and moving tank." IOP Conference Series: Materials Science and Engineering 1327, no. 1 (2025): 012104. https://doi.org/10.1088/1757-899x/1327/1/012104.

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Abstract The thermal characterisation of cryogenic fluids is quite important during their storage due to external heat leaks. Due to their low viscosity, cryogens are prone to large liquid motions w.r.t the container due to external disturbance (sloshing) during transportation. This phenomenon causes a higher internal heat generation rate due to viscous dissipation. In addition to this, the thermal stratification in the cryogenic storage container is disturbed. In the present work, as a first step, a transient two-phase thermodynamic model, for a stationary liquid nitrogen cylindrical tank, is

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3

Ustinova, A. P., Yu L. Siuskina, and R. A. Peshkov. "Evaluation of the possibility to use composite material in the structure of the rocket stage cryogenic conical tank." Proceedings of Higher Educational Institutions. Маchine Building, no. 3 (756) (March 2023): 90–100. http://dx.doi.org/10.18698/0536-1044-2023-3-90-100.

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Reducing mass of the launch vehicle components structure to increase the payload mass launched into orbit is one of the main areas in developing the space services market. Modern designs of the launch vehicles require extremely high fuel mass fraction, which necessitates introduction of the low-density materials. Fuel tanks could count for 70...80% of the total product volume, which results in the development of tanks for the cryogenic fuel obtaining decisive importance in design and development of the new type of launch vehicles. Introduction of the composite materials in designing a cryogeni

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4

Choi, Dongkuk, Sooyong Lee, and Sangwoo Kim. "A Thermodynamic Model for Cryogenic Liquid Hydrogen Fuel Tanks." Applied Sciences 14, no. 9 (2024): 3786. http://dx.doi.org/10.3390/app14093786.

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Hydrogen is used as a fuel in various fields, such as aviation, space, and automobiles, due to its high specific energy. Hydrogen can be stored as a compressed gas at high pressure and as a liquid at cryogenic temperatures. In order to keep liquid hydrogen at a cryogenic temperature, the tanks for storing liquid hydrogen are required to have insulation to prevent heat leakage. When liquid hydrogen is vaporized by heat inflow, a large pressure is generated inside the tank. Therefore, a technology capable of predicting the tank pressure is required for cryogenic liquid hydrogen tanks. In this st

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5

Johnson, W. L., R. Balasubramaniam, and R. Grotenrath. "Analysis of heat transfer from a local heat source at cryogenic temperatures." IOP Conference Series: Materials Science and Engineering 1240, no. 1 (2022): 012013. http://dx.doi.org/10.1088/1757-899x/1240/1/012013.

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Abstract Understanding the dispersion of heat around a cryogenic fluid tank, specifically the interaction between the cryogenic fluid and the tank wall is critical in the analysis of long duration cryogen storage in microgravity. The heat transfer interaction between a cryogenic storage tank and heat sources from external spacecraft structures is also one of the many factors that determine how much heat enters a tank. Recent flight experiments with two-phase fluids have indicated that local concentrations of heat input (also known as “hot spots”) can cause unwanted affects including local boil

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Klebleev, T. I., and V. Yu Semenov. "Experimental Study of Heat Transfer in the Interwall Space of a Cryogenic Tank with Powder Insulation." Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, no. 3 (146) (September 2023): 113–26. http://dx.doi.org/10.18698/0236-3941-2023-3-113-126.

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Currently, double-wall cryogenic non-isothermal tanks with vacuum-powder or vacuum-multilayer insulation are used in storage and transportation of such cryogenic liquids as liquid nitrogen, oxygen and liquefied natural gas. If the inner vessel is disrupted, the liquid spills into the heat-insulating space and evaporates as a result of heat inflow from the environment. This increases pressure in the thermal insulation space. To ensure functioning of the tank, it is necessary to limit pressure increase in the heat-insulating space. Results of experiments on evaporation of the liquid nitrogen ent

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Patil, Bhushan R., Kyle Twarog, Ossama Mannaa, and Chih-Jen Sung. "Development of test rig for optical diagnostics of cryogenic spray." IOP Conference Series: Materials Science and Engineering 1301, no. 1 (2024): 012080. http://dx.doi.org/10.1088/1757-899x/1301/1/012080.

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Abstract Spray cooling is the primary method for conducting chilldown and fill of cryogenic propellant tanks. In a typical spray injection process, a liquid sheet/jet that exits the spray nozzle undergoes primary breakup by the development of surface instabilities. Droplets and ligaments generated after the primary breakup undergo secondary breakup to create a dispersion of droplets, which extract heat on impact with the tank walls. In the existing literature, there is limited data on the primary breakup of cryogenic sprays and their detailed visualization. Moreover, an insight into the spray

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Uglanov, Dmitry, Dmitry Sarmin, Alina Akulova, Daria Aksenova, and Roman Panshin. "Thermal Cycling Toughness and Strength Estimation of Cryogenic Filled Tank." MATEC Web of Conferences 179 (2018): 01014. http://dx.doi.org/10.1051/matecconf/201817901014.

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At present, technologies based on liquid natural gas (LNG) using start to find a wide use. They also demand technologies of working fluid storage and transportation in cryogenic liquid condition. The working fluid will be used after its regasification from cryogenic liquid condition. When the gas cylinder is filled with gas, there is a danger of exceeding the temperature stresses in the cylinder walls. For the study, there is a method for calculating unsteady thermal conductivity for studying the temperature stresses in the wall of a gas cylinder during its interaction with an evaporating cryo

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Kang, Sang Guk, Myung Gon Kim, Sang Wuk Park, Chun Gon Kim, and Cheol Won Kong. "Liquid Nitrogen Storing and Pressurization Test of a Type III Cryogenic Propellant Tank." Key Engineering Materials 334-335 (March 2007): 397–400. http://dx.doi.org/10.4028/www.scientific.net/kem.334-335.397.

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Nowadays, researches for replacing material systems for cryogenic propellant tanks by composites have been being performed for the purpose of light weight of a launch vehicle. In this paper, a type III propellant tank, which is composed of the composite developed for cryogenic use and an aluminum liner, was fabricated and tested considering actual operating environment, that is, cryogenic temperature and pressure. For this aim, liquid nitrogen (LN2) was injected into the fabricated tank and in turn, gaseous nitrogen (GN2) was used for pressurization. During this test procedure, strains and tem

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Didmanidze, Otari, Alexander Afanasev, and Ramil Khakimov. "Mathematical model of the liquefied methane phase transition in the cryogenic tank of a vehicle." Journal of Mining Institute 243 (June 11, 2020): 337. http://dx.doi.org/10.31897/pmi.2020.3.337.

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In order to increase the efficiency of using vehicles (VEH) in mining and quarrying conditions, it is necessary to improve the components of gas equipment (cryogenic tank, gas nozzles, fuel supply cryogenic tubes, etc.) for supplying liquefied natural gas to the engine, as well as storage of liquid methane in a cryogenic tank with a long service life. For this, it is necessary to consider the process of heat and mass transfer of liquefied natural gas in a two-phase liquid-gas medium, taking into account the phase transition in the closed volume of the cryogenic tank under consideration.

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Dissertations / Theses on the topic "Cryogenic tank"

1

Keefer, Keaton Andrew. "DEVELOPMENT AND VALIDATION OF AN ANALYTICAL CHARGE-HOLD-VENT MODEL FOR CRYOGENIC TANK CHILLDOWN." Case Western Reserve University School of Graduate Studies / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=case1364996750.

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Mukka, Santosh Kumar. "Computation of fluid circulation in a cryogenic storage tank and heat transfer analysis during jet impingement." [Tampa, Fla.] : University of South Florida, 2005. http://purl.fcla.edu/fcla/etd/SFE0001103.

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Rao, P. Sharath Chandra. "Analysis of fluid circulation in a spherical cryogenic storage tank and conjugate heat transfer in a circular microtube." [Tampa, Fla.] : University of South Florida, 2004. http://purl.fcla.edu/fcla/etd/SFE0000461.

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Viaro, Daniele. "Numerical study of the boil-off rate in a storage tank for liquid hydrogen." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2022. http://amslaurea.unibo.it/25856/.

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A widespread rollout of alternative fuels is desirable to mitigate the issue of global warming. Hydrogen is widely considered one of the most promising solutions to reduce the environmental impact of the transport sector. This thesis work, performed in collaboration with the Norwegian University of Science and Technology NTNU, is based on the numerical study of the boil-off rate (BOR) of liquid hydrogen. The BOF represents the amount of liquid hydrogen that evaporates and that must be vented, through a pressure relief valve, in order to avoid the overpressurization of the tank. The case study

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Barsi, Stephen. "Ventless Pressure Control of Cryogenic Storage Tanks." Case Western Reserve University School of Graduate Studies / OhioLINK, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=case1283125342.

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Lozada, Luis O. "Reengineering the process of manufacturing thermal-cryogenics tanks." Online version, 2001. http://www.uwstout.edu/lib/thesis/2001/2001lozadal.pdf.

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Dannet, Grégoire. "Integration of cryogenic tanks and fuel cells for future hydrogen-powered aircraft." Thesis, Linköpings universitet, Fluida och mekatroniska system, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-176929.

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Hydrogen is seen as the green fuel of the future for the aeronautical sector allowing to reduce the carbon footprint of commercial aviation. It is well established that the release of carbon emissions triggers global warming. Aviation, like many other industries, must reduce them. This study aims to integrate cryogenic hydrogen storage onboard an existing aircraft and study two different propulsion systems, namely hydrogen combustion and fuel cells. A cryogenic tank was modelled and then designed to fit in the fuselage of an A321. Two configurations were studied, one consisting of one tank at

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Montsarrat, Christophe. "Fluid motion analysis in the cryogenic tanks of the upperstage of Ariane 5 during the ascent phase." Thesis, KTH, Aerodynamik, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-209187.

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In the frame of the improvement of the performances for Ariane 5, an analysis iscarried out to explain the pressure drop observed in the ascent phase of some flights inthe liquid hydrogen (LH2) tank of the upper stage. This stage is mainly idle until therocket is out of the atmosphere but is submitted to important excitation throughoutthe ascent phase in the atmosphere. Due to excitation, the liquid contained in thetank moves and breaks the thermodynamic equilibrium. This movement, sloshing isidentified as the most likely cause of the pressure drop observed. It is investigated inthis thesis to

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Sharifzadeh, Shayan. "Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles." Thesis, The University of Sydney, 2017. http://hdl.handle.net/2123/19127.

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Aviation industry is continuously growing especially for very long distance flights due to the globalisation of local economies around the world and the explosive economic growth in Asia. Reducing the time of intercontinental flights from 16-20 hours to 4 hours or less would therefore make the, already booming, ultra-long distance aviation sector even more attractive. To accomplish this drastic travel time reduction for civil transport, hypersonic cruise aircraft are considered as a potential cost-effective solution. Such vehicles should also be fuelled by liquid hydrogen, which is identified

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Sharifzadeh, Shayan. "Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles." Doctoral thesis, Universite Libre de Bruxelles, 2017. http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/255764.

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Aviation industry is continuously growing especially for very long distance flights due to the globalisation of local economies around the world and the explosive economic growth in Asia. Reducing the time of intercontinental flights from 16-20 hours to 4 hours or less would therefore make the, already booming, ultra-long distance aviation sector even more attractive. To accomplish this drastic travel time reduction for civil transport, hypersonic cruise aircraft are considered as a potential cost-effective solution. Such vehicles should also be fuelled by liquid hydrogen, which is identified

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Books on the topic "Cryogenic tank"

1

E, Lake R., Wilkerson C, and George C. Marshall Space Flight Center., eds. Unlined reusable filament wound composite cryogenic tank testing. National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.

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E, Lake R., Wilkerson C, and George C. Marshall Space Flight Center., eds. Unlined reusable filament wound composite cryogenic tank testing. National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.

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3

United States. National Aeronautics and Space Administration., ed. Tank pressure control in low gravity by jet mixing. National Aeronautics and Space Administration, 1993.

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4

1963-, Stephens Craig A., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Predicted thermal response of a cryogenic fuel tank exposed to simulated aerodynamic heating profiles with different cryogens and fill levels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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5

E, Anton C., and Langley Research Center, eds. Low cost, SPF aluminum cryogenic tank structure for ALS. National Aeronautics and Space Administration, Langley Research Center, 1992.

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6

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Numerical modeling of a cryogenic fluid within a fuel tank. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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7

J, Hanna Gregory, and Hugh L. Dryden Flight Research Center., eds. Thermal modeling and analysis of a cryogenic tank design exposed to extreme heating profiles. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1991.

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8

J, Hanna Gregory, and Hugh L. Dryden Flight Research Center., eds. Thermal modeling and analysis of a cryogenic tank design exposed to extreme heating profiles. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1991.

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9

Carl, Bouvier, and United States. National Aeronautics and Space Administration., eds. X-33/RLV: Reusable cryogenic tank VHM using fiber optic distributed sensing technology. National Aeronautics and Space Administration, 1998.

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Carl, Bouvier, and United States. National Aeronautics and Space Administration., eds. X-33/RLV: Reusable cryogenic tank VHM using fiber optic distributed sensing technology. National Aeronautics and Space Administration, 1998.

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Book chapters on the topic "Cryogenic tank"

1

Fornasiero, Gary R. "LNG Tank Foundation Heating Parameters." In Advances in Cryogenic Engineering. Springer US, 1986. http://dx.doi.org/10.1007/978-1-4613-2213-9_127.

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2

Greer, Donald. "Cryogenic Fuel Tank Draining Analysis Model." In Advances in Cryogenic Engineering. Springer US, 2000. http://dx.doi.org/10.1007/978-1-4615-4215-5_33.

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3

Riemer, David H. "Cryogenic Tank Stratification a Simpler Approach." In Advances in Cryogenic Engineering. Springer US, 1986. http://dx.doi.org/10.1007/978-1-4613-2213-9_107.

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Jurns, J. M., G. M. Pease, R. R. Tison, R. J. Sprafka, and R. F. Nigro. "Testing of a Buried LNG Tank." In Advances in Cryogenic Engineering. Springer US, 1998. http://dx.doi.org/10.1007/978-1-4757-9047-4_151.

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Yuan, S. W. K., and T. H. K. Frederking. "Experimental Verification of a Tank to Tank He II Transfer Model With Trade Study Results." In Advances in Cryogenic Engineering. Springer US, 1990. http://dx.doi.org/10.1007/978-1-4613-0639-9_40.

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Enya, Shintaro, and Mikio Morioka. "An Engineering Simulation of LNG Tank Rollover." In Advances in Cryogenic Engineering. Springer US, 1986. http://dx.doi.org/10.1007/978-1-4613-2213-9_128.

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7

Honkonen, Scott C., Joe R. Pietrzyk, and John R. Schuster. "Analysis of Pulsed Injection for Microgravity Receiver Tank Chilldown." In Advances in Cryogenic Engineering. Springer US, 1992. http://dx.doi.org/10.1007/978-1-4615-3368-9_60.

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Stirna, U., I. Beverte, V. Yakushin, and U. Cabulis. "Polyurethane and Polyisocyanurate Foams in External Tank Cryogenic Insulation." In Polymers at Cryogenic Temperatures. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-35335-2_10.

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Rotenberg, Y. "Numerical Simulation of Self Pressurization in a Small Cryogenic Tank." In Advances in Cryogenic Engineering. Springer US, 1986. http://dx.doi.org/10.1007/978-1-4613-2213-9_108.

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Stautner, Ernst Wolfgang, Kiruba S. Haran, Phillip J. Ansell, and Constantinos Minas. "Cryogenic Liquid Hydrogen Tank Design Aspects: General Overview." In International Cryogenics Monograph Series. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-71408-5_3.

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Conference papers on the topic "Cryogenic tank"

1

Lan, Eymon, and Shanbin Shi. "RANS-CFD Simulation of Cryogenic Tank Depressurization by Jet Induced Mixing." In Nuclear and Emerging Technologies for Space (NETS 2024). American Nuclear Society, 2024. http://dx.doi.org/10.13182/nets24-43755.

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Javia, Shailesh, and Venkat Sreenivas. "Case Study: HDD CP Retrofit for Existing Critical Service Ethylene above Ground Storage Tank." In CONFERENCE 2022. AMPP, 2022. https://doi.org/10.5006/c2022-18035.

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Abstract This case study details the retrofit installation of a replaceable linear anode based impressed current cathodic protection for a critical service double wall cryogenic Ethylene Storage Tank in Kuwait. The ground bed underneath the tank bottom has been provided with the heaters to maintain the temperature of soil, preventing the ice film formation below the tank bottom. This critical service tank could not be taken out of service and the existing CP system consisting of discreet anodes around the perimeter of the tank proved ineffective in meeting NACE criteria for cathodic protection

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BRAUN, G., W. TACK, and E. SCHOLZ. "Advanced cryogenic tank development status." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2250.

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Robinson, M. "Composite cryogenic propellant tank development." In 35th Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-1375.

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Canavan, E. R., F. K. Miller, J. G. Weisend, et al. "OPTIMIZED HEAT INTERCEPTION FOR CRYOGEN TANK SUPPORT." In ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering Conference - CEC, Vol. 52. AIP, 2008. http://dx.doi.org/10.1063/1.2908508.

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Fesmire, J. E., T. M. Tomsik, T. Bonner, et al. "Integrated heat exchanger design for a cryogenic storage tank." In ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering Conference - CEC. AIP Publishing LLC, 2014. http://dx.doi.org/10.1063/1.4860865.

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SCHOLZ, E., L. LOECHEL, and M. ROBERTS. "Advanced cryogenic propellant tank development status." In 28th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3707.

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"Development of Cryogenic Composite Tank Lined with..." In 56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.iac-05-d2.5.05.

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Yang, Hong Q., Chintan Patel, and Brandon Williams. "Validation of Cryogenic Propellant Tank Self-Pressurization." In AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-1411.

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Lavoie, J. Andre, Hongbin Shen, Amit Desai, Aaron Sechrist, and Steven Nutt. "Tenacious Composite Foams as Cryogenic Tank Insulation." In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-2090.

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Reports on the topic "Cryogenic tank"

1

Warner, M. J., D. J. Son, and D. M. Lester. 37-Inch Cryogenic Demonstration Tank. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada397863.

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2

Wu, K. C. Quench Behavior of MAGCOOL Cryogenic System with an Inline Cold Surge Tank. Office of Scientific and Technical Information (OSTI), 1991. http://dx.doi.org/10.2172/1119155.

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Lucke, R. B., and S. A. Clauss. Analysis of volatile headspace gases sampled by cryogenic traps from Westinghouse Hanford Company Tank 242-C-112 March 1992. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/10189213.

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Reed, R. P., P. T. Purtscher, N. J. Simon, et al. Aluminum alloys for ALS cryogenic tanks :. National Institute of Standards and Technology, 1993. http://dx.doi.org/10.6028/nist.ir.3979.

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5

Adams, Jesse, John Gangloff, Ned Stetson, et al. Integrated Insulation System for Cryogenic Automotive Tanks (iCAT). Office of Scientific and Technical Information (OSTI), 2018. http://dx.doi.org/10.2172/1457536.

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Cabrera, Blas, and Giorgio Gratta. Task I: Dark Matter Search Experiments with Cryogenic Detectors: CDMS-I and CDMS-II Task II: Experimental Study of Neutrino Properties: EXO and KamLAND. Office of Scientific and Technical Information (OSTI), 2013. http://dx.doi.org/10.2172/1091509.

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