Journal of Engineering for Gas Turbines and Power: Recent submissions
Now showing items 6421-6440 of 9564
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Gas Turbines in the Royal Navy
(The American Society of Mechanical Engineers (ASME), 1967) -
CODAG Propulsion Machinery by Stal-Laval for Royal Danish Navy Frigates
(The American Society of Mechanical Engineers (ASME), 1967)Two gas turbine-powered frigates for the Royal Danish Navy will go on sea trials during 1966. The CODAG propulsion units have good fuel consumption characteristics and light weight. Freewheeling ... -
Prewhirl an Added Degree of Freedom to the Designer of Small Single-Shaft Gas Turbines
(The American Society of Mechanical Engineers (ASME), 1967)The possibility of the advantageous use of adjustable guidevanes in the compressor inlet for the control of single-shaft gas turbines is discussed. Considering certain design specifications that ... -
Thrust Augmentation
(The American Society of Mechanical Engineers (ASME), 1967) -
The Effect of Vacuum Arc Remelting of Airmelt Electrodes on the Structure and Elevated Temperature Properties of a Nickel-Base Gas Turbine Superalloy
(The American Society of Mechanical Engineers (ASME), 1967)Vacuum arc remelting of electrodes prepared by the vacuum induction melting process is currently being used to provide high integrity forging billet stock of complex nickel-base superalloys. The ... -
Increasing Strength of Gas Turbine Alloys by Cold Work Prior to Aging
(The American Society of Mechanical Engineers (ASME), 1967)The combined effect of cold work and precipitation hardening treatments on the room-temperature hardness and tensile properties of A-286, Waspaloy, and Unitemp® 212 has been investigated. ... -
The Split Compressor Differential Gas Turbine Engine for Vehicle Propulsion
(The American Society of Mechanical Engineers (ASME), 1967)The performance of the vehicular split compressor differential gas turbine (SCDGT) engine is compared to that of the variable geometry free power turbine (FPT) engine. Fuel consumption, engine ... -
Long-Life Base Load Service at 1600 F Turbine Inlet Temperature
(The American Society of Mechanical Engineers (ASME), 1967)Design considerations required for base load long-life service at turbine inlet temperature above 1600 F are discussed. These include control of combustion profile, air cooling of the first-stage ... -
The Single-Blow Transient Testing Technique for Compact Heat Exchanger Surfaces
(The American Society of Mechanical Engineers (ASME), 1967)The single-blow, transient testing technique for determining the heat transfer characteristics of heat exchanger surfaces, with a summary of the underlying theory, a description of an experimental ... -
Evaluation of Heat-Resistant Alloys for Marine Gas Turbine Applications
(The American Society of Mechanical Engineers (ASME), 1967)Materials for the turbine and combustor sections of gas turbine engines were evaluated for their resistance to sulfidation corrosion. The basic evaluation was conducted in a test facility by ... -
Metallurgical Considerations Involved in the Development of Nickel-Base High-Temperature Sheet Alloys
(The American Society of Mechanical Engineers (ASME), 1967)The effects of compositional variations and the influence of production methods and heat-treatment on the properties of titanium and aluminum-hardened nickel-base alloys are described to illustrate ... -
Facilities and Instrumentation for Aircraft Engine Noise Studies
(The American Society of Mechanical Engineers (ASME), 1967)This paper describes the special facilities and instrumentation developed and used in the study of aircraft turbine-engine noise at Pratt & Whitney Aircraft. Studies of jet-exhaust noise and ... -
Discussion: “The Compact AK Process Nuclear System” (Crim, Jr., W. M., Hoffmann, J. R., and Manning, G. B., 1966, ASME J. Eng. Power, 88, pp. 127–138)
(The American Society of Mechanical Engineers (ASME), 1967) -
Discussion: “Development of the General Electric LM 1500 Gas Turbine as a Marine Power Plant” (Stoeckly, E. E., 1966, ASME J. Eng. Power, 88, pp. 144–152)
(The American Society of Mechanical Engineers (ASME), 1967) -
Discussion: “An Axial Flow Reversing Gas Turbine for Marine Propulsion” (Allen, R. P., and Butler, E. A., 1967, ASME J. Eng. Power, 89, pp. 165–170)
(The American Society of Mechanical Engineers (ASME), 1967) -
Discussion: “U. S. Navy’s Marine Gas Turbines” (Brockett, W. A., Graves, Jr., G. L., Hauschildt, M. R., and Sawyer, J. W., 1967, ASME J. Eng. Power, 89, pp. 125–143)
(The American Society of Mechanical Engineers (ASME), 1967) -
Discussion: “Gas Turbines in the Royal Navy” (Bowers, N. K., 1967, ASME J. Eng. Power, 89, pp. 95–118)
(The American Society of Mechanical Engineers (ASME), 1967) -
Discussion: “CODAG Propulsion Machinery by Stal-Laval for Royal Danish Navy Frigates” (Kumlin, Bo R. V., 1967, ASME J. Eng. Power, 89, pp. 86–93)
(The American Society of Mechanical Engineers (ASME), 1967) -
Discussion: “Thrust Augmentation” (Heiser, W. H., 1967, ASME J. Eng. Power, 89, pp. 75–81)
(The American Society of Mechanical Engineers (ASME), 1967) -
Discussion: “Increasing Strength of Gas Turbine Alloys by Cold Work Prior to Aging” (Richmond, F. M., 1967, ASME J. Eng. Power, 89, pp. 61–66)
(The American Society of Mechanical Engineers (ASME), 1967)