Книги з теми "Primary Heat Transfer System"
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Whitehouse, Adrian Paul. Heat transfer fluid in an industrial process refrigeration system. Birmingham: University of Birmingham, 1991.
Знайти повний текст джерелаC, Civinskas Kestutis, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system. [Washington, DC: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаBoyle, Robert J. Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system. [Washington, DC: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаBoyle, Robert J. Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system. [Washington, DC: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаBoyle, Robert J. Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system. [Washington, DC: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаClements, Joseph A. Heat transfer performance of a roof-spray cooling system employing the transfer function method. Springfield, Va: Available from the National Technical Information Service, 1993.
Знайти повний текст джерелаDelil, A. A. M. Test loops for two-phase thermal management system components. Amsterdam, Netherlands: National Aerospace Laboratory, 1990.
Знайти повний текст джерелаHeat transfer: Thermal management of electronics. Boca Raton: Taylor & Francis, 2010.
Знайти повний текст джерелаAbdul-Aziz, Ali. Effects of cooling system parameters on heat transfer in PAFC stack. [Washington, DC: National Aeronautics and Space Administration, 1985.
Знайти повний текст джерелаHeald, Edward E. Heat transfer: User guide for revision 5.1 : notes and exercises. Houston, PA (P.O. Box 65, Johnson Rd., Houston 15342-0065): ANSYS, 1995.
Знайти повний текст джерелаD, Quinn Robert, Gong Leslie, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Finite-element reentry heat-transfer analysis of space shuttle orbiter. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Знайти повний текст джерелаD, Quinn Robert, Gong Leslie, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Finite-element reentry heat-transfer analysis of space shuttle orbiter. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Знайти повний текст джерелаKo, William L. Finite-element reentry heat-transfer analysis of space shuttle orbiter. Edwards, Calif: Dryden Flight Research Facility, 1986.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. The embodiment design of the heat rejection system for the portable life support system. [Washington, DC: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаCenter, NAHB Research. Enerjoy case study: An evaluation of thermal comfort and energy consumption for the Energyjoy radiant panel heating system. Upper Marlboro, MD: NAHB Research Center, 1994.
Знайти повний текст джерелаCentre, Bhabha Atomic Research, ed. Characterisation of girth pipe weld for primary heat transport system of pressurised heavy water reactors. Mumbai: Bhabha Atomic Research Centre, 2002.
Знайти повний текст джерела(Firm), VBB Allen. Feasibility of energy recovery for heat pump-assisted district heating & cooling from the Metro Renton wastewater treatment plant and effluent transfer system: Phase 2 report. Salem, Or: VBB Allen, 1986.
Знайти повний текст джерелаS, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаPeck, Lindamae. Heat transfer and frost-thaw penetration in soil surrounding an inclusion of sand: Numerical model results relevant to electromagnetic sensor system performance. [Hanover, N.H]: US Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1995.
Знайти повний текст джерелаPeck, Lindamae. Heat transfer and frost-thaw penetration in soil surrounding an inclusion of sand: Numerical model results relevant to electromagnetic sensor system performance. [Hanover, N.H]: US Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1995.
Знайти повний текст джерелаPeck, Lindamae. Heat transfer and frost-thaw penetration in soil surrounding an inclusion of sand: Numerical model results relevant to electromagnetic sensor system performance. [Hanover, N.H]: US Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1995.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Effects of the cooling system parameters on heat transfer and performance of the PAFC stack during transient operation. [Cleveland, Ohio]: Cleveland State University, 1992.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Effects of the cooling system parameters on heat transfer and performance of the PAFC stack during transient operation. [Cleveland, Ohio]: Cleveland State University, 1992.
Знайти повний текст джерелаDelil, A. A. M. Sensors for a system to control the liquid flow into an evaporative cold plate of a two-phase heat transport system for large spacecraft. Amsterdam: National Aerospace Laboratory, 1986.
Знайти повний текст джерелаS, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаCavanagh, James Edward. Development of a high resolution, high heat transfer coolant system for the process control of cold strip rolling mills. Poole: Dorset Institute of Higher Education and Davy McKee (Poole) Ltd, 1985.
Знайти повний текст джерелаN, Assanis Dennis, United States. Dept. of Energy. Office of Vehicle and Engine Research and Development., and United States. National Aeronautics and Space Administration., eds. A Computer simulation of the turbocharged turbocompounded Diesel engine system: A description of the thermodynamic and heat transfer models. Washington, D.C: U.S. Dept. of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D, 1986.
Знайти повний текст джерелаH, Knoll Richard, and United States. National Aeronautics and Space Administration., eds. Thermal performance of a liquid hydrogen tank multilayer insulation system at warm boundary temperatures of 630, 530 and 152⁰ R. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаKveton, O. K. ITER cooling system: Analysis of heat transfer media, operation and safety of cooling loop and blanket during conditioning and baking. Toronto: Ontario Hydro, 1990.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаS, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаC, Ku Jerry, and United States. National Aeronautics and Space Administration., eds. Brief communication: Soot volume fraction maps for normal and reduced gravity laminar acetylene jet diffusion flames. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаC, Ku Jerry, and United States. National Aeronautics and Space Administration., eds. Brief communication: Soot volume fraction maps for normal and reduced gravity laminar acetylene jet diffusion flames. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаC, Ku Jerry, and United States. National Aeronautics and Space Administration., eds. Brief communication: Buoyancy-induced differences in soot morphology. [Washington, DC: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаSigidov, Yuriy, Elena Kalashnikova, and Tat'yana Horol'skaya. Primary accounting documentation. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1077324.
Повний текст джерелаS, Zakany James, and United States. National Aeronautics and Space Administration., eds. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаGilberto Francisco Martha de Souza. Thermal Power Plant Performance Analysis. London: Springer London, 2012.
Знайти повний текст джерелаDesideri, Umberto, Giampaolo Manfrida, and Enrico Sciubba, eds. ECOS 2012. Florence: Firenze University Press, 2012. http://dx.doi.org/10.36253/978-88-6655-322-9.
Повний текст джерелаHeat transfer: User guide for revision 5.0. Houston, PA: Swanson Analysis Systems, 1993.
Знайти повний текст джерелаShabany, Younes. Heat Transfer: Thermal Management of Electronics. Taylor & Francis Group, 2009.
Знайти повний текст джерелаShabany, Younes. Heat Transfer: Thermal Management of Electronics. Taylor & Francis Group, 2009.
Знайти повний текст джерелаFinite-element reentry heat-transfer analysis of space shuttle orbiter. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Знайти повний текст джерелаInternal thermal control system hose heat transfer fluid thermal expansion evaluation test report. Marshall Space Flight Center, Ala: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 2001.
Знайти повний текст джерелаRezk, A. M. A. Heat and Fluid Flow in Power System Components: Hmt the Science and Applications of Heat and Mass Transfer. Elsevier Science & Technology Books, 2013.
Знайти повний текст джерелаFinney, Mark, Sara McAllister, Torben Grumstrup, and Jason Forthofer. Wildland Fire Behaviour. CSIRO Publishing, 2021. http://dx.doi.org/10.1071/9781486309092.
Повний текст джерелаDesign and test of a compact optics system for the pool boiling experiment. [Washington, D.C.]: NASA, 1990.
Знайти повний текст джерелаX-34 experimental aeroheating at Mach 6 and 10. Reston, VA: American Institute of Aeronautics and Astronautics, 1998.
Знайти повний текст джерелаAnalysis of advanced solid rocket motor ignition phenomena: Final report. [Washington, DC: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаGilberto Francisco Martha de Souza. Thermal Power Plant Performance Analysis. Springer, 2014.
Знайти повний текст джерела