Books on the topic 'Gas turbine flow efficiency'

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

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

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

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

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

Arts, T. Three dimensional rotational inviscid flow calculation in axial turbine blade rows. Rhode Saint Genese, Belgium: Von Karman Institute, 1985.

Lin, Chin-Shun. Numerical calculations of turbulent reacting flow in a gas-turbine combustor. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.

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

Graham, Robert W. Recent progress in research pertaining to estimates of gas-side heat transfer in an aircraft gas turbine. [Washington, D.C.]: NASA, 1990.

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

Paxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Paxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Paxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Reynolds, R. Transition mixing study final report. [Washington, DC: National Aeronautics and Space Administration, 1986.

Vroblesky, Don A. Natural attenuation assessment of contaminated ground water at a gas-turbine manufacturing plant, Greenville, South Carolina. Columbia, S.C: U.S. Department of the Interior, U.S. Geological Survey, 1998.

Holdeman, J. D. Mixing of multiple jets with a confined subsonic crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1997.

Schmidt, Rodney C. Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades. Cleveland, Ohio: Lewis Research Center, 1988.

Lattime, Scott B. Turbine engine clearance control systems: Current practices and future directions. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Husain, Zoeb. Basic fluid mechanics and hydraulic machines. Hyderabad [India]: BS Publications, 2008.

D'Angelo, Martin. Wide speed range turboshaft study. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Zuev, Sergey, Ruslan Maleev, and Aleksandr Chernov. Energy efficiency of electrical equipment systems of autonomous objects. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1740252.

Krueger, Anne O. Xác định tỷ giá hó̂i đoái. Hà Nội: Liên Hiệp công nghệ mới, sản phả̂m mới, 1990.

E, Steinthorsson, Rigby David L, and Lewis Research Center, eds. Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Schäfer, Michael, Johannes Janicka, and AMSINI SADIKI. Flow and Combustion in Advanced Gas Turbine Combustors. Springer, 2012.

Gas Turbine Engineering Handbook, Second Edition (Incompressible Flow Turbomachines). 2nd ed. Gulf Professional Publishing, 2001.

Innovative wheel concept to increase gas turbine efficiency: Independent assessment report. [Sacramento, Calif.]: California Energy Commission, 2007.

United States. National Aeronautics and Space Administration., ed. Automotive gas turbine power system-performance analysis code. [Washington, DC]: National Aeronautics and Space Administration, 1997.

R, Chen, Cline M. C, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

R, Chen, Cline M. C, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

L, Yang S., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

L, Yang S., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

A, Hippensteele Steven, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Vidualization techniques to experimentally model flow and heat transfer in turbine and aircraft flow passages. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Griffiths, Julian P. Measurements of the flow field in a modern gas turbine combustor. 1999.

Prediction of film cooling on gas turbine airfoils. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Alexiou, Alexis. Flow and heat transfer in gas turbine H.P. compressor internal air systems. 2000.

Performance improvement through indexing of turbine airfoils. [Washington, D.C: National Aeronautics and Space Administration, 1996.

Flow and Combustion in Advanced Gas Turbine Combustors Fluid Mechanics and Its Applications. Springer, 2012.

E, Smith Clifford, Lai Ming-Chia, and Lewis Research Center, eds. Rapid mix concepts for low emission combustors in gas turbine engines. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

Razi, Nalim M., and Lewis Research Center, eds. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

United States. National Aeronautics and Space Administration., ed. Modeling improvements and users manual for axial-flow turbine off-design computer code AXOD. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Laser doppler velocimeter measurements and laser sheet imaging in an annular combustor model. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Numerical analysis of intra-cavity and power-stream flow interaction in multiple gas-turbine disk-cavities. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Urich, Dave J. An experimental investigation of soot size and flow fields in a gas turbine engine augmentor tube. 1986.

Heat transfer and flow on the first stage blade tip of a power generation gas turbine. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

C, White, and Lewis Research Center, eds. Transition mixing study final report. [Cleveland, Ohio]: Lewis Research Center, 1986.

United States. National Aeronautics and Space Administration., ed. A numerical study of the effect of wake passing on turbine blade film cooling. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

E, Smith C., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Jet mixing and emission characteristics of transverse jets in annular and cylindrical confined crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1996.