Bücher zum Thema „Test fluid“
Geben Sie eine Quelle nach APA, MLA, Chicago, Harvard und anderen Zitierweisen an
Machen Sie sich mit Top-50 Bücher für die Forschung zum Thema "Test fluid" bekannt.
Neben jedem Werk im Literaturverzeichnis ist die Option "Zur Bibliographie hinzufügen" verfügbar. Nutzen Sie sie, wird Ihre bibliographische Angabe des gewählten Werkes nach der nötigen Zitierweise (APA, MLA, Harvard, Chicago, Vancouver usw.) automatisch gestaltet.
Sie können auch den vollen Text der wissenschaftlichen Publikation im PDF-Format herunterladen und eine Online-Annotation der Arbeit lesen, wenn die relevanten Parameter in den Metadaten verfügbar sind.
Sehen Sie die Bücher für verschiedene Spezialgebieten durch und erstellen Sie Ihre Bibliographie auf korrekte Weise.
Johnston, Peter R. A survey of test methods in fluid filtration. Gulf Pub. Co., 1995.
Den vollen Inhalt der Quelle findenSteffen, Christopher J. An investigation of DTNS2D for use as an incompressible turbulence modelling test-bed. National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. A selection of experimental test cases for the validation of CFD codes. AGARD, 1994.
Den vollen Inhalt der Quelle findenNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. A selection of experimental test cases for the validation of CFD codes. AGARD, 1994.
Den vollen Inhalt der Quelle findenKasenow, Michael. Aquifer test data: Analysis and evaluation. Water Resources Publications, 2006.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. Test program, helium II, orbital resupply coupling: Final report. Ball Aerospace Systems Group, Ball Corp., 1991.
Den vollen Inhalt der Quelle findenBranstetter, J. Robert. Flight test to determine feasibility of a proposed airborne wake vortex detection concept. National Aeronautics and Space Administration, Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. Orbital transfer vehicle oxygen turbopump technology: Test series F & G, task b.8 final report. Gencorp Aeroject, Propulsion Division, 1992.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. Orbital transfer vehicle oxygen turbopump technology: Test series F&G, task b.8 final report. Gencorp Aeroject, Propulsion Division, 1992.
Den vollen Inhalt der Quelle findenJohnston, Peter R. Fluid sterilization by filtration: The filter integrity test and other filtration topics. 2nd ed. Interpharm Press, 1997.
Den vollen Inhalt der Quelle findenNeumann, Richard D. Requirements in the 1990's for high enthalpy, ground test facilities for CFD validation. American Institute of Aeronautics and Astronautics, 1990.
Den vollen Inhalt der Quelle findenJ, Motyka R., ed. Fluid geochemistry and fluid-mineral equilibria in test wells and thermal-gradient holes at the Makushin geothermal area, Unalaska Island, Alaska. State of Alaska, Dept. of Natural Resources, Division of Geological and Geophysical Surveys, 1988.
Den vollen Inhalt der Quelle findenChilds, Dara W. Design review and analysis for a Pratt & Whitney fluid-film bearing and seal testing rig: Final report. National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. Design review and analysis for a Pratt & Whitney fluid-film bearing and seal testing rig: Final report. National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenSmith, Apollo Milton Olin. Technical evaluation report on the Fluid Dynamics Panel Symposium on Aerodynamic and related hydrodynamic studies using water facilities. AGARD, 1987.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. SRM internal flow test and computational fluid dynamic analyses: Final report, contract NAS8-39095. ERC, Inc., 1995.
Den vollen Inhalt der Quelle findenMehta, Unmeel B. Synthesis of contributed simulations for OREX test cases. National Aeronautics and Space Administration, Ames Research Center, 1998.
Den vollen Inhalt der Quelle findenKopp, Robert William. Determination of the velocity, density, mass flux and enthalpy profiles for very high temperature arc jet nozzle flow. Naval Postgraduate School, 1989.
Den vollen Inhalt der Quelle findenC, Fischer Michael, and Langley Research Center, eds. F-16XL-2 supersonic laminar flow control flight test experiment. National Aeronautics and Space Administration, Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenC, Fischer Michael, and Langley Research Center, eds. F-16XL-2 supersonic laminar flow control flight test experiment. National Aeronautics and Space Administration, Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenC, Fischer Michael, and Langley Research Center, eds. F-16XL-2 supersonic laminar flow control flight test experiment. National Aeronautics and Space Administration, Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenG, Bousman William, and Ames Research Center, eds. A comparison of lifting-line and CFD methods with flight test data from a research puma helicopter. National Aeronautics and Space Administration, Ames Research Center, 1996.
Den vollen Inhalt der Quelle findenChato, David J. Review and test of chilldown methods for space-based cryogenic tanks. National Aeronautics and Space Administration, 1991.
Den vollen Inhalt der Quelle findenS, Greenberg H., Johnson S. E, and United States. National Aeronautics and Space Administration., eds. Reusable LH2 tank technology demonstration through ground test. National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenMadsen, Bjarne. Interactive computer processing and interpretation of pumping test data: A micro-computer program using dynamic graphics. Geological Survey of Denmark, Ministry of the Environment, 1985.
Den vollen Inhalt der Quelle findenAdvisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Working Group 07., ed. Test cases for inviscid flow field methods: Report of Fluid Dynamics Panel working group 07. Agard, 1985.
Den vollen Inhalt der Quelle findenS, Prahst P., and United States. National Aeronautics and Space Administration., eds. Inlet flow test calibration for a small axial compressor rig. National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenJames, Runyan L., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Lewis Icing Research Tunnel test of the aerodynamics effects of aircraft ground deicing/anti-icing fluid. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Den vollen Inhalt der Quelle findenI, Celik, Freitas Christopher J, American Society of Mechanical Engineers. Fluids Engineering Division. Spring Meeting, Canadian Society for Mechanical Engineering. Forum, and American Society of Mechanical Engineers. Fluids Engineering Division., eds. Benchmark test cases for computational fluid dynamics: Presented at the 1990 Spring Meeting of the Fluids Engineering Division held in conjunction with the 1990 Forum of the Canadian Society of Mechanical Engineers, University of Toronto, Toronto, Ontario, Canada, June 4-7, 1990. American Society of Mechanical Engineers, 1990.
Den vollen Inhalt der Quelle findenE, Walker Charlotte, and Langley Research Center, eds. Computational test cases for a rectangular supercritical wing undergoing pitching oscillations. National Aeronautics and Space Administration, Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenRoss, Hathaway, Ferguson Michael D, and Dryden Flight Research Facility, eds. Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance. National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.
Den vollen Inhalt der Quelle findenSinclair, Kirk A. A comparison of horizontal hydraulic conductivity values derived from aquifer test and well specific-capacity data for the Sequim-Dungeness area. Washington State Dept. of Ecology, 1999.
Den vollen Inhalt der Quelle findenB, Gatski T., and NASA Glenn Research Center, eds. Summary of EASM turbulence models in CFL3D with validation test cases. National Aeronautics and Space Administration, Langley Research Center, 2003.
Den vollen Inhalt der Quelle findenSorini, Susan S. Development and validation of a standard test method for sequential batch extraction of waste with acidic extraction fluid. ASTM Institute for Standards Research, 1993.
Den vollen Inhalt der Quelle findenMishra, G. C. Number of observation wells and their locations for an aquifer test in different geohydrological conditions. National Institute of Hydrology, 1993.
Den vollen Inhalt der Quelle findenE, Walker Charlotte, and Langley Research Center, eds. Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations. National Aeronautics and Space Administration, Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenMendler, O. J. Loss of feed flow, steam generator tube rupture, and steam line break thermohydraulic experiments: MB-2 steam generator transient response test program. U.S. Nuclear Regulatory Commission, 1986.
Den vollen Inhalt der Quelle findenMendler, O. J. Loss of feed flow, steam generator tube rupture, and steam line break thermohydraulic experiments: MB-2 steam generator transient response test program. U.S. Nuclear Regulatory Commission, 1986.
Den vollen Inhalt der Quelle findenMoran, Matthew E. Liquid Transfer Cryogenic Test Facility: Initial hydrogen and nitrogen no-vent fill data. NASA, 1990.
Den vollen Inhalt der Quelle findenChernecky, Cynthia C. Fluids & electrolytes. W.B. Saunders, 2002.
Den vollen Inhalt der Quelle findenScott, McRae D., Bond Ryan B, and NASA Glenn Research Center, eds. Three dimensional numerical simulation of rocket-based combined-cycle engine response during mode transition events. National Aeronautics and Space Administration, Glenn Research Center, 2003.
Den vollen Inhalt der Quelle findenLyndon B. Johnson Space Center. Systems Engineering Division. and Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services., eds. Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C). Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.
Den vollen Inhalt der Quelle finden1948-, Corrigan Ann, Alexander Mary 1955-, and Infusion Nurses Society, eds. Core curriculum for infusion nursing. 3rd ed. Lippincott Williams & Wilkins, 2004.
Den vollen Inhalt der Quelle findenAgrippa von Nettesheim, Heinrich Cornelius, 1486?-1535., Cardano Girolamo 1501-1576, Fludd Robert 1574-1637, and Parigi Silvia, eds. La magia naturale nel Rinascimento: Testi di Agrippa, Cardano, Fludd. UTET, 1989.
Den vollen Inhalt der Quelle findenKuhn, Gary D. Postflight aerothermodynamic analysis of Pegasus[copyright] using computational fluid dynamic techniques. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.
Den vollen Inhalt der Quelle findenS, Reid R., Bragg-Sitton S. M, and George C. Marshall Space Flight Center, eds. Design of refractory metal life test heat pipe and calorimeter. National Aeronautics and Space Administration, Marshall Space Flight Center, 2010.
Den vollen Inhalt der Quelle findenYudaev, Vasiliy. Hydraulics. INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/996354.
Der volle Inhalt der QuelleR, Harrivel Angela, Zimmerli Gregory A, and NASA Glenn Research Center, eds. Testing microgravity flight hardware concepts on the NASA KC-135. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Den vollen Inhalt der Quelle findenCenter, Langley Research, ed. Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle. National Aeronautics and Space Administration, Langley Research Center, 1994.
Den vollen Inhalt der Quelle finden