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Relevant bibliographies by topics / Gas turbine flow efficiency

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Academic literature on the topic 'Gas turbine flow efficiency'

Author: Grafiati

Published: 4 June 2021

Last updated: 14 February 2022

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Journal articles on the topic "Gas turbine flow efficiency"

1

Kosowski, Krzysztof, and Marian Piwowarski. "Design Analysis of Micro Gas Turbines in Closed Cycles." Energies 13, no. 21 (2020): 5790. http://dx.doi.org/10.3390/en13215790.

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The problems faced by designers of micro-turbines are connected with a very small volume flow rate of working media which leads to small blade heights and a high rotor speed. In the case of gas turbines this limitation can be overcome by the application of a closed cycle with very low pressure at the compressor inlet (lower than atmospheric pressure). In this way we may apply a micro gas turbine unit of accepted efficiency to work in a similar range of temperatures and the same pressure ratios, but in the range of smaller pressure values and smaller mass flow rate. Thus, we can obtain a gas tu

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Yang, Xiaoyong, Zhenjia Yu, Xiaoli Yu, and Jie Wang. "ICONE19-43289 EFFECTS OF FLOW LOSSES ON EFFICIENCY OF HTGR GAS TURBINE CYCLE." Proceedings of the International Conference on Nuclear Engineering (ICONE) 2011.19 (2011): _ICONE1943. http://dx.doi.org/10.1299/jsmeicone.2011.19._icone1943_125.

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Valenti, Michael. "Keeping it Cool." Mechanical Engineering 123, no. 08 (2001): 48–52. http://dx.doi.org/10.1115/1.2001-aug-2.

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This article provides details of various aspects of air cooling technologies that can give gas turbines a boost. Air inlet cooling raises gas turbine efficiency, which is proportional to the mass flow of air fed into the turbine. The higher the mass flow, the greater the amount of electricity produced from the gas burned. Researchers at Mee Industries conduct laser scattering studies of their company’s fogging nozzles to determine if the nozzles project properly sized droplets for cooling. The goal for turbine air cooling systems is to reduce the temperature of inlet air from the dry bulb temp

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Wilson, Jay M., and Henry Baumgartner. "A New Turbine for Natural Gas Pipelines." Mechanical Engineering 121, no. 05 (1999): 72–74. http://dx.doi.org/10.1115/1.1999-may-7.

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The new Cooper-Bessemer power turbine is a high-efficiency, center frame-mounted, three-stage unit that can be driven by either the existing RB211-24 gas generator or the new improved version. The upgraded gas generator combined with the new power turbine offers an increase in nominal output from 28.4 MW (38,000 hp) to 31.8 MW (42,600 hp). The new coupled turbine, now being tested, is called the Coberra 6761. Besides improving core engine performance, the program's objectives included improved fuel efficiency and reliability, and easier site serviceability; extension of the modular concept fro

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Rodgers, C. "Impingement Starting and Power Boosting of Small Gas Turbines." Journal of Engineering for Gas Turbines and Power 107, no. 4 (1985): 821–27. http://dx.doi.org/10.1115/1.3239817.

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The technology of high-pressure air or hot-gas impingement from stationary shroud supplementary nozzles onto radial outflow compressors and radial inflow turbines to permit rapid gas turbine starting or power boosting is discussed. Data are presented on the equivalent turbine component performance for convergent/divergent shroud impingement nozzles, which reveal the sensitivity of nozzle velocity coefficient with Mach number and turbine efficiency with impingement nozzle admission arc. Compressor and turbine matching is addressed in the transient turbine start mode with the possibility of oper

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Крюков, Алексей, and Aleksei Kriukov. "Three dimensional gas-dynamic calculation of nozzle block of small flow-rate centripetal turbine." Vestnik of Astrakhan State Technical University. Series: Marine engineering and technologies 2019, no. 4 (2019): 89–95. http://dx.doi.org/10.24143/2073-1574-2019-4-89-95.

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The article describes the low-consumption turbines as reliable, productive, small-sized actuating mechanisms in various units and machines. Experience in production and use  of low-cost turbine stages contributes to improving the efficiency along with simplifying and re-ducing the cost of manufacturing of the blades and the stage in general. Improving the efficiency  of low-consumption turbines requires solving the problem of aerodynamic improvement of the flow part and the calculated determination of the optimal geometry and operating modes of the impeller flow. One of the innovat

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Vidian, Fajri, Putra Anugrah Peranginangin, and Muhamad Yulianto. "Cycle-Tempo Simulation of Ultra-Micro Gas Turbine Fueled by Producer Gas Resulting from Leaf Waste Gasification." Journal of Mechanical Engineering 24, no. 3 (2021): 14–20. http://dx.doi.org/10.15407/pmach2021.03.014.

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Leaf waste has the potential to be converted into energy because of its high availability both in the world and Indonesia. Gasification is a conversion technology that can be used to convert leaves into producer gas. This gas can be used for various applications, one of which is using it as fuel for gas turbines, including ultra-micro gas ones, which are among the most popular micro generators of electric power at the time. To minimize the risk of failure in the experiment and cost, simulation is used. To simulate the performance of gas turbines, the thermodynamic analysis tool called Cycle-Te

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Rice, I. G. "Split Stream Boilers for High-Temperature/High-Pressure Topping Steam Turbine Combined Cycles." Journal of Engineering for Gas Turbines and Power 119, no. 2 (1997): 385–94. http://dx.doi.org/10.1115/1.2815586.

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Research and development work on high-temperature and high-pressure (up to 1500°F TIT and 4500 psia) topping steam turbines and associated steam generators for steam power plants as well as combined cycle plants is being carried forward by DOE, EPRI, and independent companies. Aeroderivative gas turbines and heavy-duty gas turbines both will require exhaust gas supplementary firing to achieve high throttle temperatures. This paper presents an analysis and examples of a split stream boiler arrangement for high-temperature and high-pressure topping steam turbine combined cycles. A portion of the

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Godin, T., S. Harvey, and P. Stouffs. "High-Temperature Reactive Flow of Combustion Gases in an Expansion Turbine." Journal of Turbomachinery 119, no. 3 (1997): 554–61. http://dx.doi.org/10.1115/1.2841157.

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The analysis of the chemical behavior of the working fluid in gas turbines is usually restricted to the combustion chamber sections. However, the current trend toward higher Turbine Inlet Temperatures (TIT), in order to achieve improved thermal efficiency, will invalidate the assumption of frozen composition of the gases in the first stages of the expansion process. It will become necessary to consider the recombination reactions of the dissociated species, resulting in heat release during expansion. In order to quantify the influence of this reactivity on the performance of high TIT gas turbi

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Choi, Seok Min, Seungyeong Choi, and Hyung Hee Cho. "Effect of Various Coolant Mass Flow Rates on Sealing Effectiveness of Turbine Blade Rim Seal at First Stage Gas Turbine Experimental Facility." Energies 13, no. 16 (2020): 4105. http://dx.doi.org/10.3390/en13164105.

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The appropriate coolant mass flow of turbine blade rim seal has become an important issue as turbine blades are exposed to increasingly higher thermal load owing to increased turbine inlet temperature. If the coolant is deficient, hot gas ingresses to the rim seal, or if sufficient, the efficiency of turbine decreases. Therefore, we analyzed sealing effectiveness of rim seal derive appropriate coolant mass flow rate at various conditions. The experimental facility was modified from one designed for an aero-engine gas turbine. Rotational Reynolds number varied from 3 × 105 to 5 × 105 based on r

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Dissertations / Theses on the topic "Gas turbine flow efficiency"

1

Johnson, A. B. "The aerodynamic effects of nozzle guide vane shock wave and wake on a transonic turbine rotor." Thesis, University of Oxford, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.329958.

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Plewacki, Nicholas. "Modeling High Temperature Deposition in Gas Turbines." The Ohio State University, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1587714424017527.

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Templalexis, I. K. "Gas turbine performance with distorted inlet flow." Thesis, Cranfield University, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.427101.

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Batt, J. J. M. "Three-dimensional unsteady gas turbine flow measurement." Thesis, University of Oxford, 1997. http://ora.ox.ac.uk/objects/uuid:3302ca8f-0618-4440-9e23-3bf99bc3705d.

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The high pressure turbine stage can be considered the most important component for the efficiency and longevity of a modern gas turbine. The flow field within this stage is highly complex and is both unsteady and three-dimensional. Understanding this flow field is essential if improvements are to be made to future engine designs. Increasingly designers are placing more emphasis on the use of Computational Fluid Dynamics (CFD) rather than experimental results. CFD methods can be more flexible and cost effective. However before these predictions can be used they must be validated against experim

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Palafox, Pepe. "Gas turbine tip leakage flow and heat transfer." Thesis, University of Oxford, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.427699.

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Stitzel, Sarah M. "Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine." Thesis, Virginia Tech, 2001. http://hdl.handle.net/10919/30992.

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The current demands for higher performance in gas turbine engines can be reached by raising combustion temperatures to increase thermal efficiency. Hot combustion temperatures create a harsh environment which leads to the consideration of the durability of the combustor and turbine sections. Improvements in durability can be achieved through understanding the interactions between the combustor and turbine. The flow field at a combustor exit shows non-uniformities in pressure, temperature, and velocity in the pitch and radial directions. This inlet profile to the turbine can have a considerable

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Hollis, David. "Particle image velocimetry in gas turbine combustor flow fields." Thesis, Loughborough University, 2004. https://dspace.lboro.ac.uk/2134/7640.

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Current and future legislation demands ever decreasing levels of pollution from gas turbine engines, and with combustor performance playing a critical role in resultant emissions, a need exists to develop a greater appreciation of the fundamental causes of unsteadiness. Particle Image Velocimetry (PIV) provides a platform to enable such investigations. This thesis presents the development of PIV measurement methodologies for highly turbulent flows. An appraisal of these techniques applied to gas turbine combustors is then given, finally allowing a description of the increased understanding of

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Alhajeri, Hamad. "Heat removal in axial flow high pressure gas turbine." Thesis, Cranfield University, 2016. http://dspace.lib.cranfield.ac.uk/handle/1826/11465.

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The demand for high power in aircraft gas turbine engines as well as industrial gas turbine prime mover promotes increasing the turbine entry temperature, the mass flow rate and the overall pressure ratio. High turbine entry temperature is however the most convenient way to increase the thrust without requiring a large change in the engine size. This research is focused on improving the internal cooling of high pressure turbine blade by investigating a range of solutions that can contribute to the more effective removal of heat when compared with existing configuration. The role played by the

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Janakiraman, S. V. "Fluid flow and heat transfer in transonic turbine cascades." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-06112009-063614/.

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Ghulam, Mohamad. "Characterization of Swirling Flow in a Gas Turbine Fuel Injector." University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1563877023803877.

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Books on the topic "Gas turbine flow efficiency"

1

Janicka, Johannes. Flow and Combustion in Advanced Gas Turbine Combustors. Springer Netherlands, 2013.

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Janicka, Johannes, Amsini Sadiki, Michael Schäfer, and Christof Heeger, eds. Flow and Combustion in Advanced Gas Turbine Combustors. Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5320-4.

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Shyy, W. A numerical study of flow in gas-turbine combustor. AIAA, 1987.

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4

Standardization, International Organization for. Measurement of gas flow in closed conduits - turbine meters. International Organization for Standardization, 1993.

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5

Hermsmeyer, Stephan. Improved methods for modelling turbine engine gas flow properties. University of Birmingham, 1996.

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6

Arts, T. Three dimensional rotational inviscid flow calculation in axial turbine blade rows. Von Karman Institute, 1985.

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7

Lin, Chin-Shun. Numerical calculations of turbulent reacting flow in a gas-turbine combustor. National Aeronautics and Space Administration, 1987.

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8

G, Williams J. Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows. National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.

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9

Graham, Robert W. Recent progress in research pertaining to estimates of gas-side heat transfer in an aircraft gas turbine. NASA, 1990.

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10

Gorla, Rama S. R. Probabilistic analysis of solid oxide fuel cell based hybrid gas turbine system. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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Book chapters on the topic "Gas turbine flow efficiency"

1

Siegmann, J., G. Becker, J. Michaelis, and M. Schäfer. "Efficient Numerical Schemes for Simulation and Optimization of Turbulent Reactive Flows." In Flow and Combustion in Advanced Gas Turbine Combustors. Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5320-4_10.

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Ulbrich, S., and R. Roth. "Efficient Numerical Multilevel Methods for the Optimization of Gas Turbine Combustion Chambers." In Flow and Combustion in Advanced Gas Turbine Combustors. Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5320-4_13.

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Zohuri, Bahman. "Gas Turbine Working Principles." In Combined Cycle Driven Efficiency for Next Generation Nuclear Power Plants. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-15560-9_7.

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Zohuri, Bahman, and Patrick McDaniel. "Gas Turbine Working Principals." In Combined Cycle Driven Efficiency for Next Generation Nuclear Power Plants. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-70551-4_7.

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Chow, S. K., D. G. N. Tse, and J. H. Whitelaw. "Review of Recent Measurements in Gas Turbine Combustors." In Combustings Flow Diagnostics. Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2588-8_14.

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Rieger, Neville F. "Flow Efficiency and Excitation in Turbine Stages." In Vibration and Wear in High Speed Rotating Machinery. Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-1914-3_24.

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Schobeiri, Meinhard T. "Turbine and Compressor Cascade Flow Forces." In Gas Turbine Design, Components and System Design Integration. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-23973-2_5.

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Schobeiri, Meinhard T. "Turbine and Compressor Cascade Flow Forces." In Gas Turbine Design, Components and System Design Integration. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-58378-5_5.

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Schobeiri, Meinhard T. "Efficiency of Multi-Stage Turbomachines." In Gas Turbine Design, Components and System Design Integration. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-23973-2_7.

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Schobeiri, Meinhard T. "Efficiency of Multi-Stage Turbomachines." In Gas Turbine Design, Components and System Design Integration. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-58378-5_7.

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Conference papers on the topic "Gas turbine flow efficiency"

1

Schlein, Barry. "Gas Turbine Combustion Efficiency." In ASME 1985 Beijing International Gas Turbine Symposium and Exposition. American Society of Mechanical Engineers, 1985. http://dx.doi.org/10.1115/85-igt-121.

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A method of correlating combustor efficiency as a function of geometry and operating conditions is presented. A simple equation correlates all the data for a given engine type with a single parameter. The correlating parameter is a function of fuel flow, pressure, temperature and volume in a form similar to others in the literature. The unique feature of the correlating parameter is its use of internal gas temperature rather than the commonly used combustor inlet temperature. The result is an equation requiring an iterative solution since combustion efficiency is a part of the correlating para

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Shobhavathy, M. T., and Premakara Hanoca. "CFD Analysis to Understand the Flow Behaviour of a Single Stage Transonic Axial Flow Compressor." In ASME 2013 Gas Turbine India Conference. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gtindia2013-3592.

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This paper comprises the Computational Fluid Dynamic (CFD) analysis to investigate the flow behaviour of a high speed single stage transonic axial flow compressor. Steady state analyses were carried out at design and part speed conditions to obtain the overall performance map using commercial CFD software ANSYS FLUENT. Radial distribution of flow parameters were obtained at 90% of design speed for the choked flow and near stall flow conditions. The predicted data were validated against available experimental results. The end wall flow fields were studied with the help of velocity vector plots

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Arcoumanis, C., I. Hakeem, L. Khezzar, R. F. Martinez-Botas, and N. C. Baines. "Performance of a Mixed Flow Turbocharger Turbine Under Pulsating Flow Conditions." In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/95-gt-210.

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The performance of a high pressure ratio (P.R.=2.9) mixed flow turbine for an automotive turbocharger has been investigated and the results revealed its better performance relative to a radial-inflow geometry under both steady and pulsating flow conditions. The advantages offered by the constant blade angle rotor allow better turbocharger-engine matching and maximization of the energy extracted from the pulsating engine exhaust gases. In particular, the mixed inlet blade geometry resulted in high efficiency at high expansion ratios where the engine-exhaust pulse energy is maximum. The efficien

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Rajamani, Keerthivasan, Madhu Ganesh, Karthikeyan Paramanandam, et al. "Cooling Efficiency Enhancement Using Impingement Cooling Technique for Turbine Blades." In ASME 2013 Gas Turbine India Conference. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gtindia2013-3803.

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The effect of impingement cooling on the internal surface (cooling passage) of the leading edge region in a commercial turbine high pressure first stage rotor blade is investigated using Computational Fluid Dynamics (CFD) simulations. The flow domain is obtained by stretching the middle cross section (50% span) of the above mentioned blade. The simulations are performed for 3 different profiles in the cooling flow passage. In all the cases, the nozzle position and Mach number of cooling fluid is kept constant at E/D = 4.32 and 0.4 respectively. In the first case, the suction side profile is mo

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Banerjee, Abhisek, Sukanta Roy, Prasenjit Mukherjee, and Ujjwal K. Saha. "Unsteady Flow Analysis Around an Elliptic-Bladed Savonius-Style Wind Turbine." In ASME 2014 Gas Turbine India Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/gtindia2014-8141.

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Although considerable progress has already been achieved in the design of wind turbines, the available technical designs are not yet adequate to develop a reliable wind energy converter especially meant for small-scale applications. The Savonius-style wind turbine appears to be particularly promising for the small-scale applications because of its design simplicity, good starting ability, insensitivity to wind directions, relatively low operating speed, low cost and easy installation. However, its efficiency is reported to be inferior as compared to other wind turbines. Aiming for that, a numb

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Dominy, Robert G., David A. Kirkham, and Andrew D. Smith. "Flow Development Through Inter-Turbine Diffusers." In ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-gt-139.

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Inter-turbine diffusers offer the potential advantage of reducing the flow coefficient in the following stages leading to increased efficiency. The flows associated with these ducts differ from those in simple annular diffusers both as a consequence of their high-curvature S-shaped geometry and of the presence of wakes created by the upstream turbine. Experimental data and numerical simulations clearly reveal the generation of significant secondary flows as the flow develops through the diffuser in the presence of cross-passage pressure gradients. The further influence of inlet swirl is also d

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Moyle, Ian N. "Analysis of Efficiency Sensitivity Associated With Tip Clearance in Axial Flow Compressors." In ASME 1988 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1988. http://dx.doi.org/10.1115/88-gt-216.

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The effects of tip clearance changes on efficiency in axial compressors are typically established experimentally. The ratio of change of efficiency with change of clearance gap varies significantly for different compressors in the published data. An analysis of this sensitivity range in terms of the blade and stage design parameters was initiated. The analysis revealed that the sensitivity range largely resulted from a derivation at constant flow of the efficiency decrement. It was also found that a generalized loss method of generating the sensitivities produced a much improved correlation of

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Krzyzanowski, J. A. "On Predicting Steam Turbine Blading Erosion and Turbine Efficiency Deterioration." In ASME 1988 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1988. http://dx.doi.org/10.1115/88-gt-224.

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Two-phase flow of wet steam is nowadays a subject of intensive research for different reasons. Prediction of erosion damage to turbine blading is one of important elements of this research. In the paper, a method of predicting this damage as a function of time is presented briefly. The emphasis is however put on the statistics of the accuracy of damage prediction as compared to field measurements. Also comments on erosion induced turbine efficiency deterioration are presented. The paper relates to the authors experience presented in references [1] and [2].

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Prasad, Santosh Kumar, Pradeep Sangli, Osman Buyukisik, and Dave Pugh. "Prediction of Gas Turbine Oil Scoop Capture Efficiency." In ASME 2014 Gas Turbine India Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/gtindia2014-8329.

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The lubrication system in a gas turbine engine is akin to the human blood circulatory system. Providing right quantities of oil to the right components for cooling and lubrication is the primary function of the lubrication system. In the current analysis, at the downstream end of the lube oil supply line, a stationary oil nozzle sprays a jet of oil to a high speed rotating component called an oil scoop. The function of the oil scoop which rotates at speeds usually greater than 10000 RPM is to ‘Scoop’ or capture the oil and provide an under race oil transfer mechanism to the bearings rotating e

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Patel, Kashyap, Chaina Ram, and Vishal Rasaniya. "Numerical Analysis of Turbulent Mixing in Cross Flow Configurations." In ASME 2019 Gas Turbine India Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gtindia2019-2506.

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Abstract The gas turbine combustion chamber is a vital part of a gas turbine engine. Proper mixing of air in the combustor plays an important role in combustion. Increasing mixing rate is an important factor for better combustion efficiency. The injection of air in crossflow is widely studied over the years. The air injected at an angle in upstream direction gives better mixing by colliding with the crossflow. The computational analysis of the injected jet in cross flow is performed with different angles in the upstream direction. The k-omega SST turbulence model was used to investigate the mi

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Reports on the topic "Gas turbine flow efficiency"

1

Dr. Adam London. A Low-Cost, High-Efficiency Periodic Flow Gas Turbine for Distributed Energy Generation. Office of Scientific and Technical Information (OSTI), 2008. http://dx.doi.org/10.2172/932510.

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Norris, Thomas R. Test Program for High Efficiency Gas Turbine Exhaust Diffuser. Office of Scientific and Technical Information (OSTI), 2009. http://dx.doi.org/10.2172/969712.

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W.L. Lundberg, G.A. Israelson, M.D. Moeckel, et al. A High Efficiency PSOFC/ATS-Gas Turbine Power System. Office of Scientific and Technical Information (OSTI), 2001. http://dx.doi.org/10.2172/859228.

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Steward, W. Gene. Flow Integrating Section for a Gas Turbine Engine in Which Turbine Blades are Cooled by Full Compressor Flow. Office of Scientific and Technical Information (OSTI), 1999. http://dx.doi.org/10.2172/764563.

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Wang, Anbo, Gary Pickrell, Russell May, and Adrian Roberts. High Temperature Optical Fiber Instrumentation for Gas Flow Monitoring in Gas Turbine Engines. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada400148.

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K.R. Rajagopal and I.J. Rao. AN INVESTIGATION INTO THE MECHANICS OF SINGLE CRYSTAL TURBINE BLADES WITH A VIEW TOWARDS ENHANCING GAS TURBINE EFFICIENCY. Office of Scientific and Technical Information (OSTI), 2006. http://dx.doi.org/10.2172/887494.

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Hsu, M., D. Nathanson, and D. T. Bradshaw. ZTEK`s ultra-high efficiency fuel cell/gas turbine system for distributed generation. Office of Scientific and Technical Information (OSTI), 1996. http://dx.doi.org/10.2172/460195.

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Detor, Andrew, Richard DiDomizio, Don McAllister, Erica Sampson, Rongpei Shi, and Ning Zhou. A New Superalloy Enabling Heavy Duty Gas Turbine Wheels for Improved Combined Cycle Efficiency. Office of Scientific and Technical Information (OSTI), 2017. http://dx.doi.org/10.2172/1337871.

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Solomon, P. R., Yuxin Zhao, and D. S. Pines. Feasibility study for an advanced coal fired heat exchanger/gas turbine topping cycle for a high efficiency power plant. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/7089854.

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Solomon, P. R., Y. Zhao, D. Pines, R. C. Buggeln, and S. J. Shamroth. Feasibility study for an advanced coal fired heat exchanger/gas turbine topping cycle for a high efficiency power plant. Final report. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/10135308.

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