Technical Literature Digest

Optimization of Power-Plant and Airplane Performance—a Symposium. Aeronautical Engineering Review, vol. 13, June 1954, pp. 42-56. The Compound Aero Engine, by E. E. Chatterton, Aeronautics, vol. 30, June 1954, pp. 61-62, 67-68, 71. Characteristics of a Vaporizing Combustor for Aviation Gas Turbines, by W. D. Pouchot and J. R. Hamm, Trans. ASME, vol. 76, July 1954, pp. 801-807. Contribution to the Study of Axial Supersonic Compressors, by Pierre Schwaar, ZAMP, vol. 5, Mar. 15, 1954, pp. 13615 (in French). Applications of Dimensional Analysis to Spray-Nozzle Performance Data, by R. Shafer and Harry L. Bovey, / . Res. Nat. Bur. Stand., vol. 52, March 1954, pp. 141-147. Gas Turbine Starters for Jet Engines, by L. R. Neurlin and F . W. Fernald, Aviation Age, vol. 21, May 1954, pp. 138146. The Future of the Turbo Compound Engine, by Russell R. Mock and Norton B. Jamieson, Mechanical Engineering, vol. 76, May 1954, pp. 603-606. Helicopter's Hopes Lifted by Turboprops, by Robert M. Loebelson, Amer. Aviation, vol. 18, July 5, 1954, pp. 15-16. Anglo-American Jewel (Description of the Wright J-65 Sapphire), Flight, vol. 65, June 18, 1954, pp. 787-788. Turbo-Wasp Dissected (Prat t and Whitney J-57), Flight, vol. 65, May 14, 1954, pp.619-620. Compression Ignition Gas Turbine (Napier Nomad), by C. D. Carmichael, Shell Aviation News, No. 192, June 1954, pp. 16-20. Gas Turbines for Helicopters, by H, C. Maskey, Continental Aviation and Engng. Corp., Feb. 1954, 17 pp. Experiments on Model Thrust Reversers for Jet Aircraft, by M. A. Hiatt , Boeing AircraflCo. Document No. D-15077, March 1954, Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine. I. Methods for Determining Heat Transfer Characteristics, by H. H. Ellerbrock and R. R. Ziemer. I I . Methods for Determining Cooling-Air Flow Characteristics, by H. H. Ellerbrock. I I I . Methods for Determining Power and Efficiency, by H. H. Ellerbrock I I I , and R. R. Ziemer, NACA RM E50A05, and E50A06, Jan. 1950, and E50E18, May 1950. (Declassified 1953) Effect of Air Distribution on Radial Temperature Distribution in One-Sixth Sector of Annular Turbojet Combustor, by Herman Mark and Eugene V. Zettle, NACA R M E9L22, Sept. 1949. (Declassified 1953) Radiant Heat Transfer From Flames in a Singule Tubular Turbojet Combustor, by Leonard Topper, NACA R M E52F23, June 1952. (Declassified 1953) Comparison of Outside-Surface HeatTransfer Coefficients For Cascades of Turbine Blades, by James E. Hubbart, NACA R M E50C28, March 1950. (Declassified 1953) Heat Transfer and Operating Characteristics of Aluminum Forced-Convection and Stainless-Steel Natural Convection Water-Cooled Single-Stage Turbines, by John C. Freche and A. J. Diaguila, NACA R M E50DO3a, April 1950. (Declassified 1953) Analytical Investigation of Flow and Heat Transfer in Coolant Passages of Free-Convection Liquid Cooled Turbines, by E. R. G. Eckert and Thomas W. Jackson, NACA R M E50D25, April 1950. (Declassified 1953) Numerical Solution of Equations for One-Dimensional Gas Flow in Rotating Coolant Passages, by W. Byron Brown and Richard J. Rossbacb, NACA R M E50E04, May 1950. (Declassified 1953) Extension of Boundary Layer Heat Transfer Theory to Cooled Turbine Blades, by W. Byron Brown and Patrick L. Donoughe, NACA R M E50F02, June 1950. (Declassified 1953) Analytical Determination of Local Surface Heat Transfer Coefficients For Cooled Turbine Blades From Measured Metal Temperatures, by W. Byron Brown and Jack B. Esgar, NACA R M E50F09, June 1950. (Declassified 1953) Determination of Gas-to-Blade Convection Heat-Transfer Coefficients on a Forced Convection, Water Cooled Singlestage Aluminum Turbine, by John C. Freche and Eugene F . Schum, NACA R M E50J23, Oct., 1950. (Declassified 1953) Average Outside-Surface Heat-Transfer Coefficients and Velocity Distributions For Heated and Cooled Impulse Turbine Blades in Static Cascades, by James E. Hubbart and Eugene F. Schum, NACA R M E50L20, Dec. 1950. (Declassified 1953) Determination of Blade to Coolant Heat Transfer Coefficients on a Forced Convection, Water-Cooled, Single-Stage Turbine, by John C. Freche and Eugene F. Schum, NACA R M E51E18, May 1951. (Declassified 1953) Calculations of Laminar Heat Transfer Around Cylinders of Arbitrary Cross Section and Transpiration Cooled Walls With Application To Turbine Blade Cooling, by E. R. G. Eckert and John N. B. Livingood, NACA R M E51F22, June 1951. (Declassified 1953) Blade to Coolant Heat Transfer Results and Operating Data From a Natural Convection Water Cooled Single-Stage Turbine, by Anthony J. Diaguila and John C. Freche, NACA R M E51I17, Sept. 1951. (Declassified 1953) Experimental Investigation of CoolantFlow Characteristics of a Sintered Porous Turbine Blade, by Edward R. Bartoo, Louis J. Schafer, Jr., and Hadley T. Richards, NACA R M E51K02, Nov. 1951. (Declassified 1953) Experimental Investigation of the HeatTransfer Characteristics of an Air-Cooled Sintered Porous Turbine Blade, by Louis J. Schafer, Jr., Edward R. Bartoo, and Hadley T. Richards, NACA R M E51K08, Nov. 1951. (Declassified 1953) Pressure Drop in Coolant Passages of Two Air-Cooled Turbine Blade Configurations, by W. Byron Brown and Henry O. Slone, NACA R M E52D01, April 1952. (Declassified 1953) Comparison of Calculated and Experimental Temperatures of Water-Cooled Turbine Blades, by Eugene F . Schum, John C. Freche, and William J. Stelpflug, NACA R M E52D21, April 1952. (Declassified 1953) Analytical Investigation of Two Liquid Cooling Systems For Turbine Blades, by Thomas W. Jackson and John N. B. Livingood, NACA R M E51F04, June 1951. (Declassified 1953) Experimental Investigation of AirCooled Turbine Blades in Turbojet Engine. X-Endurance Evaluation of Several TubeFilled Rotor Blades, by Jack B. Esgar and John L. Clure, NACA R M E52B13, Feb. 1952. (Declassified 1953)