Journal of Engineering for Gas Turbines and Power: Recent submissions
Now showing items 2701-2720 of 9564
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Residual Stresses in Gas Turbine Engine Components From Barkhausen Noise Analysis
(The American Society of Mechanical Engineers (ASME), 1974) -
A Three-Dimensional Theory for Calculating Circulation in Axial Turbomachines (Direct Problems)
(The American Society of Mechanical Engineers (ASME), 1974)In this work the steady-state spanwise circulation distribution of thin, slightly cambered radial blades of finite length is calculated using the method of singularities. The analysis extends the ... -
Discussion: “End-Wall Boundary Layers in Axial Compressors” (Hirsch, Ch., 1974, ASME J. Eng. Power, 96, pp. 413–426)
(The American Society of Mechanical Engineers (ASME), 1974) -
Torsional Stability Analysis of a Gas-Turbine Powered Helicopter Drive System
(The American Society of Mechanical Engineers (ASME), 1974)The torsional stability of a closed-loop dynamic system is evaluated. The system is a typical transport helicopter speed governor, gas-turbine engine and drive train. This is compared with the ... -
Discussion: “The M.I.T. Blowdown Compressor Facility” (Kerrebrock, J. L., Epstein, A. H., Haines, D. M., and Thompkins, W. T., 1974, ASME J. Eng. Power, 96, pp. 394–405)
(The American Society of Mechanical Engineers (ASME), 1974) -
Heat Transfer and Film Cooling Following Normal Injection Through a Round Hole
(The American Society of Mechanical Engineers (ASME), 1974)Heat transfer is measured downstream of perpendicular injection of an air jet through a single hole into a turbulent mainstream boundary layer. The heat transfer coefficient, calculated from ... -
A Potassium-Steam Binary Vapor Cycle for Better Fuel Economy and Reduced Thermal Pollution
(The American Society of Mechanical Engineers (ASME), 1973)Both fuel supply and thermal pollution considerations that are becoming progressively more important strongly favor the development of a higher temperature, and more efficient, thermodynamic cycle ... -
Low Pressure Ratio Fan Noise Experiment and Theory
(The American Society of Mechanical Engineers (ASME), 1973)The Q-FAN™, a new low pressure ratio, low noise propulsor, is currently under intensive development. Since the operating regime of the Q-FAN differs from that of the turbofan, the dominant ... -
Corrosion of Metals by Liquid Vanadium Pentoxide and the Sodium Vanadates
(The American Society of Mechanical Engineers (ASME), 1973)The rates of liquid vanadate corrosion of iron, nickel and several alloys containing iron, nickel, and chromium have been examined by the use of both static and dynamic accelerated corrosion ... -
Corrosion and Deposits From Combustion of Solid Waste
(The American Society of Mechanical Engineers (ASME), 1973)Combustion of solid waste in municipal incinerators has resulted in fouling and corrosion on heat transfer surfaces. The nature of these deposits and the extent of the corrosion has been ... -
Performance of MONEL Alloy 400 in Feedwater Heaters
(The American Society of Mechanical Engineers (ASME), 1973)With access to data on more than thirty years service experience with MONEL alloy 400 tubing in high-pressure feedwater heaters, the Huntington Alloy Products Division conducted an extensive ... -
Discussion: “Lift and Pressure Fluctuations of a Cambered Airfoil Under Periodic Gusts and Applications in Turbomachinery” (Naumann, H., and Yeh, H., 1973, ASME J. Eng. Power, 95, pp. 1–10)
(The American Society of Mechanical Engineers (ASME), 1973) -
Perspectives for Waste Heat Recovery by Means of Organic Fluid Cycles
(The American Society of Mechanical Engineers (ASME), 1973)Organic compounds, employed as working fluids for low temperature heat recovery, are shown to exhibit a performance better than that of steam cycles. The potential influence on efficiency and ... -
Thermal Stresses and Initial Deformation of Heated Condenser Tubes
(The American Society of Mechanical Engineers (ASME), 1973)A condenser tube bank with individual tubes axially and laterally restrained at the ends by tube sheets, and laterally restrained at intermediate locations by support plates is subjected to a ... -
Gas Velocity Measurements Within a Compressor Rotor Passage Using the Laser Doppler Velocimeter
(The American Society of Mechanical Engineers (ASME), 1973)The laser Doppler velocimeter, a new instrument capable of making nondisturbing gas velocity measurements, was used to investigate the flowfield within the rotating blade row of a low speed ... -
Experiences of a Multiple Gas Turbine Machinery in Fast Patrol Craft
(The American Society of Mechanical Engineers (ASME), 1973)The Swedish Spica-class torpedo boats have been in service now for some years. The experiences of the craft are reported good and some details are given in this paper of the results with ... -
An Investigation of the Contribution of Solar Energy in Heating Greenhouses in Quebec
(The American Society of Mechanical Engineers (ASME), 1973)An experimental study on a commercial greenhouse in Montréal, Québec, was undertaken during the winter season, October 1971–April 1972. The object of the study was to determine the percentage ... -
Further Development of the Burning Profile
(The American Society of Mechanical Engineers (ASME), 1973)In 1967, Messrs, Wagoner and Duzy presented a paper at the Winter Annual Meeting of the ASME entitled “Burning Profiles for Solid Fuels”, in which they described a derivative thermogravimetric ... -
Pollutants From Methane Fueled Gas Turbine Combustion
(The American Society of Mechanical Engineers (ASME), 1973)In view of the greater flexibility of a gas turbine combustion system design as compared to that for a piston engine, control of NOx emissions even while keeping the CO and hydrocarbon ... -
Modelling of Gas Turbine Combustors; Considerations of Combustion Efficiency and Stability
(The American Society of Mechanical Engineers (ASME), 1973)The stability and combustion efficiency performance of gas turbine combustion chambers is examined with relation to correlation groups derived from a reaction rate equation obtained in earlier ...