Aircraft gas-turbines -- Blades -- Cooling -- Mathematical models
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An analysis of the capabilities and limitations of turbine air cooling methods (National Aeronautics and Space Administration ;, 1970), by Jack B. Esgar, Albert Kaufman, Raymond S. Colladay, and Lewis Research Center (page images at HathiTrust)
Items below (if any) are from related and broader terms.
Filed under: Aircraft gas-turbines -- Blades -- Cooling- Incidence loss for a core turbine rotor blade in a two-dimensional cascade (National Aeronautics and Space Administration ;, 1974), by Roy G. Stabe, John F. Kline, and Lewis Research Center (page images at HathiTrust)
- Cold-air annular-cascade investigation of aerodynamic performance of cooled turbine vanes (National Aeronautics and Space Administration ;, 1974), by Louis J. Goldman, Kerry L. McLallin, and Lewis Research Center (page images at HathiTrust)
- Aerodynamic performance of a ceramic-coated core turbine vane tested with cold air in a two-dimensional cascade (National Aeronautics and Space Administration ;, 1975), by Roy G. Stabe, Curt H. Liebert, and Lewis Research Center (page images at HathiTrust)
- Comparison of cooling effectiveness of turbine vanes with and without film cooling (National Aeronautics and Space Administration ;, 1974), by Frederick C. Yeh and Lewis Research Center (page images at HathiTrust)
- Metal temperatures and coolant flow in a wire-cloth transpiration-cooled turbine vane (National Aeronautics and Space Administration ;, 1975), by Herbert J. Gladden (page images at HathiTrust)
- Turbine vane coolant flow variations and calculated effects on metal temperatures (National Aeronautics and Space Administration ;, 1975), by Frederick C. Yeh, Louis M. Russell, Peter L. Meitner, and Lewis Research Center (page images at HathiTrust)
- Aerodynamic performance of a fully film cooled core turbine vane tested with cold air in a two-dimensional cascade (National Aeronautics and Space Administration ;, 1975), by Roy G. Stabe, John F. Kline, and Lewis Research Center (page images at HathiTrust)
- Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), by Charles F. Zalabak, Arthur N. Curren, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- An analysis of the capabilities and limitations of turbine air cooling methods (National Aeronautics and Space Administration ;, 1970), by Jack B. Esgar, Albert Kaufman, Raymond S. Colladay, and Lewis Research Center (page images at HathiTrust)