최소 단어 이상 선택하여야 합니다.
최대 10 단어까지만 선택 가능합니다.
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기Aerospace science and technology, v.93, 2019년, pp.105327 -
Li, Jiachao (School of Astronautics, Beihang University) , Liang, Guozhu (School of Astronautics, Beihang University) , Zhu, Pingping (Beijing Institute of Astronautical Systems Engineering) , Wang, Xi (Beijing Institute of Astronautical Systems Engineering)
Abstract In order to accurately predict the whole operating process of a liquid hydrogen tank under gaseous hydrogen pressurization, a 2-D axial symmetry Volume-of-Fluid (VOF) based numerical simulation method is established. Phase change and turbulence models are included in the numerical simulati...
Olsen 1996 Experimental and Analytical Investigation of Interfacial Heat and Mass Transfer in a Pressurized Tank Containing Liquid Hydrogen
Dewitt 1966 Experimental Evaluation of Pressurant Gas Injectors During the Pressurized Discharge of Liquid Hydrogen
Adv. Cryog. Eng. Gluck 7 219 1962 Gas requirements in pressurized transfer of liquid hydrogen
Stochl 1969 Gaseous-Hydrogen Requirements for the Discharge of Liquid Hydrogen From a 1.52-Meter-(5-FT) Diameter Spherical Tank
Stochl 1969 Gaseous-Hydrogen Requirements for the Discharge of Liquid Hydrogen From a 3.96-Meter-(13-FT-) Diameter Spherical Tank
Stochl 1970 Gaseous-Helium Requirements for the Discharge of Liquid Hydrogen From a 1.52-Meter-(5-FT-) Diameter Spherical Tank
Ludwig 2012 Analyses of Cryogenic Propellant Tank Pressurization Based Upon Ground Experiments
Cryogenics Ludwig 63 1 2014 10.1016/j.cryogenics.2014.05.005 Investigations on thermodynamic phenomena of the active-pressurization process of a cryogenic propellant tank
Stewart 2017 Pressurization of a Flightweight, Liquid Hydrogen Tank: Evaporation & Condensation at the Liquid/Vapor Interface
Thompson 1965 Prediction of Propellant Tank Pressurization Requirements by Dimensional Analysis
Aerosp. Sci. Technol. Yang 82 83 161 2018 10.1016/j.ast.2018.09.008 Investigation on self-pressurization and ignition performance of nitrous oxide fuel blend ethylene thruster
Holt 2000 Numerical Modeling and Test Data Comparison of Propulsion Test Article Helium Pressurization Sys-Tem
J. Propuls. Power Majumdar 17 2 385 2001 10.2514/2.5754 Numerical modeling of pressurization of a propellant tank
Roudebush 1965 An Analysis of the Problem of Tank Pressurization During Outflow
Masters 1974 Computer Programs for Pressurization (RAMP) and Pressurized Expulsion From a Cryogenic Liquid Propellant Tank
J. Thermophys. Heat Transf. Daigle 27 1 116 2013 10.2514/1.T3933 Temperature stratification in a cryogenic fuel tank
J. Spacecr. Rockets Kwon 49 6 1150 2012 10.2514/1.A32073 Modeling the prediction of helium mass requirement for propellant tank pressurization
Aerosp. Sci. Technol. Torras 84 75 2019 10.1016/j.ast.2018.10.010 Multiphysics modeling and experimental validation of low temperature accumulator for cryogenic space propulsion systems
Hardy 1990 Prediction of the Ullage Gas Thermal Stratification in a NASP Vehicle Propellant Tank Experimental Simulation Using Flow-3D
Sasmal 1991 Computational Modeling of the Pressurization Process in a NASP Vehicle Propellant Tank Experi-Mental Simulation
Hirt 1988 Flow-3D User's Manual
Adnani 2000 Pressurization Analysis of Cryogenic Propulsion Systems
Adv. Cryog. Eng. Schmidt 487 1960 An experimental study concerning the pressurization and stratification of liquid hydrogen
Appl. Therm. Eng. Joseph 111 1629 2017 10.1016/j.applthermaleng.2016.07.015 Effect of insulation thickness on pressure evolution and thermal stratification in a cryogenic tank
Cryogenics Wang 57 63 2013 10.1016/j.cryogenics.2013.05.005 CFD investigation of thermal and pressurization performance in LH2 tank during discharge
Int. J. Heat Mass Transf. Wang 62 263 2013 10.1016/j.ijheatmasstransfer.2013.03.021 Transient thermal and pressurization performance of LO2 tank during helium pressurization combined with outside aerodynamic heating
Aerosp. Sci. Technol. Liu 85 544 2019 10.1016/j.ast.2019.01.005 Hydrodynamic performance in a sloshing liquid oxygen tank under different initial liquid filling levels
Microgravity Sci. Technol. Chen 25 4 203 2013 10.1007/s12217-013-9340-2 Simulation research of vaporization and pres-sure variation in a cryogenic propellant tank at the launch site
Yang 2015 CFD Extraction of Heat Transfer Coefficient in Cryogenic Propellant Tanks
J. Comput. Phys. Hirt 39 1 201 1981 10.1016/0021-9991(81)90145-5 Volume of fluid (VOF) method for the dynamics of free boundaries
Aerosp. Sci. Technol. Agarwal 32 1 60 2014 10.1016/j.ast.2013.12.001 Prediction of gas-core vortices during draining of liquid propellants from tanks
J. Beijing Univ. Aeronaut. Astronaut. Li 44 1 99 2018 Experiment and numerical simulation of liquid nitrogen tank atmospheric ground parking
J. Astronaut. Li 39 4 426 2018 Experiment and numerical simulation of liquid nitrogen tank self-pressurization
J. Fluid Mech. Panzarella 484 41 2003 10.1017/S0022112003004002 On the validity of purely thermodynamic descriptions of two-phase cryogenic fluid storage
J. Sci. Comput. Yakhot 1 1 3 1986 10.1007/BF01061452 Renormalization group analysis of turbulence. I. Basic theory
Int. J. Heat Mass Transf. Henkes 2 34 377 1991 10.1016/0017-9310(91)90258-G Natural convection flow in a square cavity calculated with low-Reynolds-number turbulence models
Chem. Rev. Persad 116 14 7727 2016 10.1021/acs.chemrev.5b00511 Expressions for the evaporation and condensation coefficients in the Hertz-Knudsen relation
Chem. Rev. Davidovits 106 4 1323 2006 10.1021/cr040366k Mass accommodation and chemical reactions at gas-liquid interfaces
Aerosol Sci. Technol. Mozurkewich 5 2 223 1986 10.1080/02786828608959089 Aerosol growth and the condensation coefficient for water: a review
Knudsen 1934 The Kinetic Theory of Gases: Some Modern Aspects
Schrage 1953 A Theoretical Study of Interphase Mass Transfer
Ann. Phys. Hertz 253 10 177 1882 10.1002/andp.18822531002 Ueber die verdunstung der flussigkeiten, insbesondere des quecksilbers, im luftleeren raume
J. Colloid Interface Sci. Barrett 150 2 352 1992 10.1016/0021-9797(92)90205-Z Kinetic evaporation and condensation rates and their coefficients
Int. J. Heat Mass Transf. Labuntsov 22 7 989 1979 10.1016/0017-9310(79)90172-8 Analysis of intensive evaporation and condensation
Haynes 2010 CRC Handbook of Chemistry and Physics
Lee 407 1980 Multiphase Transport: Fundamentals, Reactor Safety, Applications A pressure iteration scheme for two-phase flow modeling
Comput. Chem. Eng. Schepper 33 1 122 2009 10.1016/j.compchemeng.2008.07.013 Modeling the evaporation of a hydrocarbon feedstock in the convection section of a steam cracker
Int. J. Heat Mass Transf. Kryukov 54 13-14 3042 2011 10.1016/j.ijheatmasstransfer.2011.02.042 About evaporation-condensation coefficients on the vapor-liquid interface of high thermal conductivity matters
Alberts 2016 Numerical Approach to Measure Accommodation Coefficients for Long-Duration Spaceflight Cryogenic Propellants
Int. J. Heat Mass Transf. Wu 50 5-6 1186 2007 10.1016/j.ijheatmasstransfer.2006.10.013 Simulation of refrigerant flow boiling in serpentine tubes
Appl. Therm. Eng. Liu 112 801 2017 10.1016/j.applthermaleng.2016.10.124 Thermodynamic performance of pre-pressurization in a cryogenic tank
Wang vol. 1 36 2018 Computational research on phase change model for cryogenic propellant in microgravity
Asia-Pac. J. Chem. Eng. Wang 9 1 63 2014 10.1002/apj.1746 Numerical investigation of pressurization performance in cryogenic tanks of new-style launch vehicle
Chin. J. Aeronaut. Li 2019 10.1016/j.cja.2019.05.008 Simulation of the mass and heat transfer in liquid hydrogen tanks during pressurization
NIST Chemistry WebBook, NIST standard reference database, October 2011 release, available from: http://webbook.nist.gov/chemistry/.
Dresar 1993 Pressurization and Expulsion of a Flight Weight Liquid Hydrogen Tank
Zilliac 2005 Modeling of Propellant Tank Pressurization
Int. Adv. Cryogenic Eng. Clark 10 259 1964 A review of pressurization, stratification and interfacial phenomena
*원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.