Книги з теми "Jet impingement heat transfer"

Cooper, Leonard Y. Ceiling jet properties and wall heat transfer in compartment fires near regions of ceiling jet-wall impingement. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, National Engineering Laboratory, Center for Fire Research, 1986.

Impingement jet cooling in gas turbines. Boston, MA: WIT Press, 2014.

Nunn, Robert H. Jet vane heat transfer modeling. Monterey, California: Naval Postgraduate School, 1986.

Hemeson, Anthony Onyekwere. Influence of burner design on impingement heat transfer from flames. Portsmouth: Portsmouth Polytechnic, Dept. of Mechanical Engineering, 1986.

Hatzenbuehler, Mark A. Modeling of jet vane heat-transfer characteristics and simulation of thermal response. Monterey, California: Naval Postgraduate School, 1988.

D.C.) International Heat Transfer Conference (14th 2010 Washington. Enhancement of heat transfer with pool and spray impingement boiling on microporous and nanowire surface coatings. Golden, CO: National Renewable Energy Laboratory, 2010.

S, Samuelsen G., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Jet mixing in a reacting cylindrical crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

S, Samuelsen G., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Jet mixing in a reacting cylindrical crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

C, Su C., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Heat transfer characteristics within an array of impinging jets: Effects of crossflow temperature relative to jet temperature. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

P, Proctor Margaret, and United States. National Aeronautics and Space Administration., eds. Transient technique for measuring heat transfer coefficients on stator airfoils in a jet engine environment. [Washington, DC: National Aeronautics and Space Administration, 1985.

J, Santoro Gilbert, and Lewis Research Center, eds. Determination of convective diffusion heat/mass transfer rates to burner rig test targets comparable in size to cross-stream jet diameter. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

James, VanFossen G., and Lewis Research Center, eds. The influence of jet-grid turbulence on heat transfer from the stagnation region of a cylinder in crossflow. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

James, VanFossen G., and Lewis Research Center, eds. The influence of jet-grid turbulence on heat transfer from the stagnation region of a cylinder in crossflow. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

James, VanFossen G., and Lewis Research Center, eds. The influence of jet-grid turbulence on heat transfer from the stagnation region of a cylinder in crossflow. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

A, Gokoglu Suleyman, and Lewis Research Center, eds. Experiments for the determination of convective diffusion heat/mass transfer to burner rig test targets comparable in size to jet stream diameter. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Murthy, S. N. B. WINCOF-I code for prediction of fan compressor unit with water ingestion. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

Murthy, S. N. B. WINCOF-I code for prediction of fan compressor unit with water ingestion. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

Li, Tong, Greenberg Paul S, and United States. National Aeronautics and Space Administration., eds. Measurements and modeling of soot formation and radiation in microgravity jet diffusion flames. [Washington, DC: National Aeronautics and Space Administration, 1996.

Li, Tong, Greenberg Paul S, and United States. National Aeronautics and Space Administration., eds. Measurements and modeling of soot formation and radiation in microgravity jet diffusion flames. [Washington, DC: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Gas-jet and tangent-slot film cooling tests of a 12.5⁰ cone at Mach number of 6.7. [Washington, DC]: National Aeronautics and Space Administration, 1988.

United States. National Aeronautics and Space Administration., ed. Gas-jet and tangent-slot film cooling tests of a 12.5⁰ cone at Mach number of 6.7. [Washington, DC]: National Aeronautics and Space Administration, 1988.

C, 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.

C, 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.

L, Yang S., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

R, Chen, Cline M. C, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

R, Chen, Cline M. C, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

L, Yang S., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

C, 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.

Dulke, Michael F. Heat transfer modeling of jet vane Thrust Vector Control (TVC) Systems. 1987.

Heat Transfer Between a Plane Surface and a Pulsating, Perpendicularly Impinging Air Jet. Creative Media Partners, LLC, 2021.

WINCOF-I code for prediction of fan compressor unit with water ingestion. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

Gas-jet and tangent-slot film cooling tests of a 12.5⁰ cone at Mach number of 6.7. [Washington, DC]: National Aeronautics and Space Administration, 1988.