Książki na temat „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 i United States. National Aeronautics and Space Administration., red. Jet mixing in a reacting cylindrical crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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

C, Su C., i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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, i United States. National Aeronautics and Space Administration., red. 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, i Lewis Research Center, red. 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., i Lewis Research Center, red. 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., i Lewis Research Center, red. 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., i Lewis Research Center, red. 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, i Lewis Research Center, red. 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 i United States. National Aeronautics and Space Administration., red. 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 i United States. National Aeronautics and Space Administration., red. 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., red. 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., red. 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, i United States. National Aeronautics and Space Administration., red. 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, i United States. National Aeronautics and Space Administration., red. 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., i United States. National Aeronautics and Space Administration., red. 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 i United States. National Aeronautics and Space Administration., red. 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 i United States. National Aeronautics and Space Administration., red. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

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

C, Ku Jerry, i United States. National Aeronautics and Space Administration., red. 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.