Books on the topic 'Turbomachinery aerodynamics'

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Unsteady aerodynamic phenomena in turbomachines. Neuilly sur Seine, France: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Unsteady aerodynamic phenomena in turbomachines. Neuilly-sur-Seine: AGARD, 1990.

Verdon, Joseph M. Unsteady aerodynamic models for turbomachinery aeroelastic and aeroacoustic applications. Cleveland, Ohio: Lewis Research Center, 1995.

Chen, Naixing. Aerothermodynamics of turbomachinery: Analysis and design. Hoboken, N.J: Wiley, 2010.

Schobeiri, Meinhard. Turbomachinery flow physics and dynamic performance. 2nd ed. New York: Springer, 2012.

Schobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. 2nd ed. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.

Montgomery, Matthew D. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

M, David. TIGGERC--turbomachinery interactive grid generator for 2-D grid applications and uers guide. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

King, Paul I. Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery: Final report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

King, Paul I. Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery: Final report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

S, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. [Washington, DC]: National Aeronautics and Space Administration, 1994.

S, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. [Washington, DC: National Aeronautics and Space Administration, 1991.

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. Cleveland, Ohio: Lewis Research Center, 1989.

E, Cunningham Robert. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Cunningham, Robert E. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Cunningham, Robert E. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. Cleveland, Ohio: Lewis Research Center, 1986.

Rao, J. S. Turbomachine unsteady aerodynamics. New Delhi: Wiley Eastern, 1994.

Boretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. Cleveland, Ohio: Lewis Research Centre, 1990.

Boretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.

Boretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.

International, Symposium on Unsteady Aerodynamics Aeroacoustics and Aeroelasticity of Turbomachines (11th 2006 Moscow Russia). Turbomachines: Aeroelasticity, aeroacoustics, and unsteady aerodynamics. [Moscow]: Torus Press, 2006.

Fransson, Torsten H., ed. Unsteady Aerodynamics and Aeroelasticity of Turbomachines. Dordrecht: Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-011-5040-8.

Hall, Kenneth C., Robert E. Kielb, and Jeffrey P. Thomas, eds. UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES. Dordrecht: Kluwer Academic Publishers, 2006. http://dx.doi.org/10.1007/1-4020-4605-7.

Kurkov, Anatole P. Measurement of gust response on a turbine cascade. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Atassi, H. M., ed. Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers. New York, NY: Springer New York, 1993. http://dx.doi.org/10.1007/978-1-4613-9341-2.

Atassi, H. M. Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers. New York, NY: Springer New York, 1993.

Fransson, Torsten H. Unsteady Aerodynamics and Aeroelasticity of Turbomachines: Proceedings of the 8th International Symposium held in Stockholm, Sweden, 14-18 September 1997. Dordrecht: Springer Netherlands, 1998.

Propulsion, and Energetics Panel Specialists' Meeting (68th 1986 Munich Germany). Transonic and supersonic phenomena in turbomachines: Papers presented at the Propulsion and Energetics 68th(B) Specialists' Meeting, held in Munich, Germany, 10-12 September 1986. Neuilly-sur-Seine, France: AGARD, 1987.

V, Subramanian S. Application of Runge Kutta time marching scheme for the computation of transonic flows in turbomachines. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Murthy, S. N. B. Transient performance of fan engine with water ingestion. [Washington, DC]: National Aeronautics and Space Administration, U.S. Dept. of Transportation, Federal Aviation Administration, 1993.

Vsesoi͡uznai͡a, konferent͡sii͡a po aėrouprugosti turbomashin (11th 1987 Uz͡hhorod Ukraine). XI Vsesoi͡uznai͡a konferent͡sii͡a po aėrouprugosti turbomashin: G. Uzhgorod, 15-17 sent. 1987 g. : tezisy dokladov. Kiev: IPP AN USSR, 1987.

Dickinson, Wayne. A benthic chamber with electric stirrer mixing. Woods Hole, Mass: Woods Hole Oceanographic Institution, 1992.

T, Fransson, ed. Unsteady aerodynamics and aeroelasticity of turbomachines: Proceedings of the 8th international symposium held in Stockholm, Sweden, 14-18 September 1997. Dordrecht: Kluwer Academic, 1998.

ASME. Print Proceedings of the ASME Turbo Expo 2018 : Turbomachinery Technical Conference and Exposition : Volume 2B : Turbomachinery : Axial Flow Turbine Aerodynamics; Turbomachinery : Noise, Ducts and Interactions; Turbomachinery: Radial Turbomachinery Aerodynamics. American Society of Mechanical Engineers, The, 2018.

Center, Lewis Research, ed. A review of turbomachinery blade-row interaction research. Cleveland, Ohio: Lewis Research Center, National Aeronautics and Space Administration, 1988.

Max, Platzer, Carta Franklin O, North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel., and North Atlantic Treaty Organization. Advisory Groupfor Aerospace research and Development. Structures and Materials Panel., eds. AGARD manual on aeroelasticity in axial-flow turbomachines. Volume 1: Unsteady turbomachinery aerodynamics. Neuilly sur Seine, France: AGARD, 1987.

Asme Turbo Expo: Electric Power, Turbomachinery. American Society of Mechanical Engineers, 2004.

1939-, Sieverding C. H., Hodson H. P, and Von Karman Institute for Fluid Dynamics., eds. Blade row interference effects in axial turbomachinery stages: February 9-12, 1998. Rhode St. Genèse, Belgium: Von Karman Institute for Fluid Dynamics, 1998.

ASME. Print Proceedings of the ASME Turbo Expo 2018 : Turbomachinery Technical Conference and Exposition : Volume 2A : Turbomachinery : Axial Flow Fan and Compressor Aerodynamics; Turbomachinery: Unsteady Flows in Turbomachinery. American Society of Mechanical Engineers, The, 2018.

Application of a lower-upper implicit scheme and an interactive grid generation for turbomachinery flow field simulations. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Woo-Yung, Soh, Yoon Seokkwan, and United States. National Aeronautics and Space Administration., eds. Application of a lower-upper implicit scheme and an interactive grid generation for turbomachinery flow field simulations. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Application of a lower-upper implicit scheme and an interactive grid generation for turbomachinery flow field simulations. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Woo-Yung, Soh, Yoon Seokkwan, and United States. National Aeronautics and Space Administration., eds. Application of a lower-upper implicit scheme and an interactive grid generation for turbomachinery flow field simulations. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Schobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. Springer, 2008.

Asme Turbo Expo: Microturbines and Small Turbomachinery, Structures and Dynamics. American Society of Mechanical Engineers, 2004.

Center, Lewis Research, ed. Validation of viscous and inviscid computational methods for turbomachinery components. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, DC]: National Aeronautics and Space Administration, 1996.

A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, DC]: National Aeronautics and Space Administration, 1996.

M, Verdon Joseph, and United States. National Aeronautics and Space Administration., eds. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, DC]: National Aeronautics and Space Administration, 1996.