Books on the topic 'Hot flows'

Nagabushana, K. A. Heat transfer from cylinders in subsonic slip flows. Hampton, Va: Langley Research Center, 1992.

Nagabushana, K. A. Heat transfer from cylinders in subsonic slip flows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Stainback, P. Calvin. Fluctuation diagrams for hot-wire anemometry in subsonic compressible flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Logan, P. Uncertainties in hot-wire measurements of compressible turbulent flows implied by comparisons with laser-induced fluorescence. New York: AIAA, 1986.

Pitts, William M. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

Pitts, William M. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

Pitts, William M. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

Pitts, William M. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

Arab, Rupert Fazal. Statistical analysis of hot-wire calibration coefficients for normal and inclined wires in heated turbulent flows. Ottawa: National Library of Canada, 1995.

Aichouni, Mohamed. Development and decay of turbulent pipe flows: An experimental and computational study. Salford: Universityof Salford, 1992.

Pitts, William M. Chemically reacting turbulent flow. Gaithersburg, MD: U.S. Dept. of Commerce, National Bureau of Standards, 1986.

Pitts, William M. Chemically reacting turbulent flow. Gaithersburg, MD: U.S. Dept. of Commerce, National Bureau of Standards, 1986.

Rosemann, Henning. Einfluss der Geometrie von Mehrfach-Hitzdrahtsonden auf die Messergebnisse in turbulenten Stromungen. Koln: DLR, 1989.

Doiron, M. D. Turbulent flow measurements with a triple-split hot-film probe. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.

Clauser, Christoph, ed. Numerical Simulation of Reactive Flow in Hot Aquifers. Berlin, Heidelberg: Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-642-55684-5.

Shirtliffe, CJ, and RP Tye, eds. Guarded Hot Plate and Heat Flow Meter Methodology. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1985. http://dx.doi.org/10.1520/stp879-eb.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. Hampton, Va: Langley Research Center, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. Washington D.C: National Aeronautics and SpaceAdministration, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Doiron, Michael Donald. Attached and separated trailing edge flow measurements with a triple-split hot-film probe. [Toronto, Ont.]: University of Toronto, Graduate Department of Aerospace Science and Engineering, 1992.

Seymour, M. J. Cold downdraughts: Application guide 2/91. Bracknell: Building Services Research and Information Association, 1992.

Fisher, Michael J. A modelling of the noise from simple coaxial jets. Part III - With hot primary flow. Southampton, England: University of Southampton, Institute of Sound and Vibration Research, 1994.

Khalid, M. The use of hot-film technique for boundary layer studies on a 21% thick airfoil. Ottawa: National Aeronautical Establishment, 1987.

Khalid, M. The use of hot-film technique for boundary layer studies on a 21% thick airfoil. Ottawa: NationalResearch Council Canada, 1987.

Parrott, Tony L. Pressure probe and hot-film probe response to acoustic excitation in mean flow. Hampton, Va: Langley Research Center, 1986.

Doiron, Michael Donald. Attached and separated trailing edge flow measurements with a triple-split hot-film probe. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1993.

Westbye, Christopher John. Flow boiling heat transfer in the quenching of a hot tube under microgravity conditions. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1993.

Robinson, Raymond C. Hot corrosion test facility at the NASA Lewis Special Projects Laboratory. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Brok, Sebastianus Willem Josef den. An experimental investigation into the effect of water on the flow of quartzite =: Experimenteel onderzoek naar het effekt van water op het vloeigedrag van kwartsiet. [Utrecht: Faculteit Aardwetenschappen der Rijksuniversiteit te Utrecht, 1992.

Xu, Jason Jianxin. Flow boiling heat transfer in the quenching of a hot surface under reduced gravity conditions. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1998.

Boutazakhti, Mohamed. The effect of jet mixing on the combustion efficiency of a hot, fuel-rich cross-flow. Ottawa: National Library of Canada, 2000.

Miller, Robert T. Cyclic injection, storage, and withdrawal of heated water in a sandstone aquifer at St. Paul, Minnesota: Analysis of thermal data and nonisothermal modeling of short-term test cycles. Mounds View, Minn: U.S. Geological Survey, 1994.

Laser anemometry techniques for hot flows. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Farrar, Brian. Hot film anemometry in dispersed oil-water flows. Bradford, 1988.

Magnus, Axelsson, ed. Cool discs, hot flows: The varying faces of accreting compact objects : Funäsdalen, Sweden 25-30 March 2008. Melville, N.Y: American Institute of Physics, 2008.

Magnus, Axelsson, ed. Cool discs, hot flows: The varying faces of accreting compact objects : Funäsdalen, Sweden 25-30 March 2008. Melville, N.Y: American Institute of Physics, 2008.

Magnus, Axelsson, ed. Cool discs, hot flows: The varying faces of accreting compact objects : Funäsdalen, Sweden 25-30 March 2008. Melville, N.Y: American Institute of Physics, 2008.

Henny J. G. L. M. Lamers (Editor) and A. Sapar (Editor), eds. Thermal & Ionization Aspects of Flows from Hot Stars, Observations & Theory: Proceedings of a Workshop Held in Tartu, Estonia, 23-27 August, 1999 (Astronomical ... Society of the Pacific Conference Series). Astronomical Society of the Pacific, 2000.

Escudier, Marcel. Engineering applications of Bernoulli’s equation. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0008.

Clauser, Christoph. Numerical Simulation of Reactive Flow in Hot Aquifers. Springer, 2014.

B, Roebuck, and National Physical Laboratory (Great Britain), eds. Measuring flow stress in hot axisymmetric compression tests. Teddington: NPL, 1997.

Ruban, Anatoly I. Boundary-Layer Separation. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199681754.003.0003.

United States. National Aeronautics and Space Administration., ed. Hot wire anemometer measurements in the unheated air flow tests of the SRB nozzle-to-case joint: Final report. [Washington, DC: National Aeronautics and Space Administration, 1989.

United States. National Aeronautics and Space Administration., ed. Flowfield visualization for SSME hot gas manifold: Final report. Huntsville, AL: Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center, 1988.

J, Shirtliffe C., Tye R. P, ASTM Committee C-16 on Thermal Insulation., and National Research Council of Canada., eds. Guarded hot plate and heat flow meter methodology: A symposium. Philadelphia, PA: ASTM, 1985.