Books on the topic 'Jet impingement heat transfer'

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1

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.

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2

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

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3

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

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4

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

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5

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

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6

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.

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7

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.

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8

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.

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9

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.

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10

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.

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11

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.

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12

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.

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13

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.

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14

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.

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15

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.

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16

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.

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17

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.

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18

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.

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19

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.

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20

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.

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21

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.

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22

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.

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23

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.

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24

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.

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25

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.

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26

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.

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27

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.

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28

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.

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29

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

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30

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

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31

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

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32

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.

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