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Combustion chambers -- Materials -- Cooling

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• Combustion chambers -- Materials
• Combustion chambers -- Cooling

• Combustion chambers -- Cooling -- Materials

• Simultaneous film and convection cooling of a plate inserted in the exhaust stream of a gas turbine combustor (National Aeronautics and Space Administration ;, 1973), by Cecil J. Marek, Albert J. Juhasz, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Reliability and effective thermal conductivity of three metallic-ceramic composite insulating coatings on cooled hydrogen-oxygen rockets (National Aeronautics and Space Administration ;, 1973), by Harold G. Price, Richard J. Quentmeyer, Ralph L. Schacht, and Lewis Research Center (page images at HathiTrust)

• Conventionally cast and forged copper alloy for high-heat-flux thrust chambers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by John M. Kazaroff, George A. Repas, and Lewis Research Center (page images at HathiTrust)

• High-temperature durability considerations for HSCT combustor (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Nathan S. Jacobson and Lewis Research Center (page images at HathiTrust)

• Jet model for slot film cooling with effect of free-stream and coolant turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Frederick F. Simon and Lewis Research Center (page images at HathiTrust)
• Turbulent heat-transfer prediction method for application to scramjet engines (National Aeronautics and Space Administration ;, 1974), by S. Z. Pinckney and Langley Research Center (page images at HathiTrust)
• Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure (National Aeronautics and Space Administration ;, 1967), by Arthur N. Curren and Lewis Research Center (page images at HathiTrust)

• Measurements of liner cooling effectiveness within a full-scale double-annular ram-induction combustor (National Aeronautics and Space Administration ;, 1974), by Edward J. Mularz, Donald F. Schultz, and U.S. Army Air Mobility Research and Development Laboratory (page images at HathiTrust)

• Effect of free-stream turbulence on film cooling (National Aeronautics and Space Administration ;, 1975), by Cecil J. Marek, Robert R. Tacina, and Lewis Research Center (page images at HathiTrust)
• Film cooling in a combustor operating at fuel-rich exit conditions (National Aeronautics and Space Administration ;, 1974), by Robert R. Tacina, Cecil J. Marek, and Lewis Research Center (page images at HathiTrust)