Discussion: “The Exhaust-Heated Gas-Turbine Cycle” (Mordell, D. L., 1950, Trans. ASME, 72, pp. 323–326) [PDF]
, 1950 D. G. Shepherd
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Nonconventional Technologies Review, 2020 The objective of the paper is concerning an 8 axis Adaptive Robotic System GTAW welding on 3,2 mm thickness test piece, base material stainless steel 304L with 1,2 mm diameter ER308L as filler material.
Andrei Mitru +2 more
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Measurement of the Temperature Distribution in the Disc of Gas Turbines by Electrical Tank Method
, 1950 Shiro Nukiyama
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Intrinsic aeroacoustic instabilities in the crosstalk apertures of can-annular combustors [PDF]
arXivThis paper presents an experimental and numerical study of aeroacoustic instabilities at the interface between neighbouring combustion chambers in modern heavy-duty gas turbines. A simplified laboratory-scale geometry of the gap separating the outlet of these chambers, just upstream of the turbine inlet in can-annular combustor architectures, is ...
arxiv
INVESTIGATION OF HEAT-RESISTING STEEL FOR GAS TURBINES (III)
, 1954 Sadao Koshiba, Tsuneo Kuno
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Experimental Pressure Gain Analysis of Pulsed Detonation Engine
AerospaceA pulsed detonation chamber (PDC) equipped with Hartmann–Sprenger resonators has been designed and tested for both Hydrogen/air and Hydrogen/Oxygen mixtures.
Alina Bogoi +5 more
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Discussion: “Gas Turbines and Turbosuperchargers” (Moss, Sanford A., 1944, Trans. ASME, 66, pp. 351–363) [PDF]
, 1944 W. F. Durand
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Closure to “Discussions of ‘Design and Operation of Some Experimental High-Temperature Gas-Turbine Units’” (1947, Trans. ASME, 69, p. 558) [PDF]
, 1947 A. D. Hughes
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Progress report to Materials Laboratory, Wright Air Development Center, Department of the Air Force on four low-alloy steels for rotor disks of gas turbines in jet engines [PDF]
, 1951 R. L. Jones +2 more
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