Books on the topic 'Turbomachinery flow'
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Schobeiri, Meinhard T. Turbomachinery Flow Physics and Dynamic Performance. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-24675-3.
Full textSchobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. Berlin, Heidelberg: Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/b137854.
Full textSchobeiri, Meinhard. Turbomachinery flow physics and dynamic performance. 2nd ed. New York: Springer, 2012.
Find full textSchobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. 2nd ed. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.
Find full textTurbomachinery flow physics and dynamic performance. Berlin: Springer, 2005.
Find full textCaughey, D. A. Multigrid calculation of three-dimensional turbomachinery flows. Ithaca, New York: Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University, 1989.
Find full textMontgomery, 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.
Find full textLepicovsky, Jan. Use of pressure sensitive paint for diagnostics in turbomachinery flows with shocks. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2000.
Find full textChung-hua, Wu. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Find full textChung-hua, Wu. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Find full textS, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Find full textS, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. [Washington, DC: National Aeronautics and Space Administration, 1991.
Find full textSteinke, 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.
Find full textSteinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. Cleveland, Ohio: Lewis Research Center, 1989.
Find full textJoint, ASCE/ASME Mechanics Conference (1985 Albuquerque N. M. ). Design methods for two-phase flow in turbomachinery: Presented at the ASCE/ASME Mechanics Conference, Albuquerque, New Mexico, June 24-26, 1985. New York, N.Y. (345 E. 47th St., New York 10017): American Society of Mechanical Engineers, 1985.
Find full textConference, Joint ASCE/ASME Mechanics. Design methods for two-phase flow in turbomachinery: Presented at the ASCE/ASME Mechanics Conference, Albuquerque, New Mexico, June 24-26, 1985. New York, N.Y. (345 E. 47th St., New York 10017): American Society of Mechanical Engineers, 1985.
Find full textKurkov, Anatole P. Measurement of gust response on a turbine cascade. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Find full textBoretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. Cleveland, Ohio: Lewis Research Centre, 1990.
Find full textEscudier, Marcel. Flow through axial-flow-turbomachinery blading. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0014.
Full textToledo-Velázquez, Miguel, and Fabrizio Fontaneto. Developments in Turbomachinery Flow. Excelic Press LLC, 2018.
Find full textDevelopments in Turbomachinery Flow. Elsevier, 2015. http://dx.doi.org/10.1016/c2014-0-03018-3.
Full textSchobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. Springer, 2008.
Find full textSchobeiri, Meinhard T. Turbomachinery Flow Physics and Dynamic Performance. Springer London, Limited, 2006.
Find full textSchobeiri, Meinhard T. Turbomachinery Flow Physics and Dynamic Performance. Springer Berlin / Heidelberg, 2010.
Find full textSchobeiri, Meinhard T. Turbomachinery Flow Physics and Dynamic Performance. Springer, 2016.
Find full textTurbomachinery design and tonal acoustics computations. San Jose, CA: MCAT Institute, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. PIV for turbomachinery applications. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Find full textNumerical simulation of complex turbomachinery flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textB, Lakshminarayana, and NASA Glenn Research Center, eds. Numerical simulation of complex turbomachinery flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textMax, 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.
Find full textASME. 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.
Find full textK, Choo Yung, Eiseman Peter R, Reno Charles J, and Lewis Research Center, eds. Interactive grid generation for turbomachinery flow field simulations. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1988.
Find full textMontazerin, Nader, Ghasem Akbari, and Moastafa Mahmoodi. Developments in Turbomachinery Flow: Forward Curved Centrifugal Fans. Elsevier Science & Technology, 2015.
Find full textMontazerin, Nader, Ghasem Akbari, and Mostafa Mahmoodi. Developments in Turbomachinery Flow: Forward Curved Centrifugal Fans. Elsevier Science & Technology, 2015.
Find full textUnited States. National Aeronautics and Space Administration, ed. Multigrid calculation of three-dimensional turbomachinery flows. Ithaca, New York: Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University, 1989.
Find full textASME. 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.
Find full textCenter, Lewis Research, ed. Validation of viscous and inviscid computational methods for turbomachinery components. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textThe design/analysis of flows through turbomachinery: A viscous/inviscid approach. [Washington, D.C.]: NASA, 1991.
Find full textCenter, Lewis Research, and United States. Army Aviation Systems Command., eds. Computer code for predicting coolant flow and heat transfer in turbomachinery. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textA, Mulac Richard, Celestina Mark L, and Lewis Research Center, eds. A model for closing the inviscid form of the average-passage equation system. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textLi, Eric L. A parallel multigrid method for predicting compressible flow in turbomachinery. 2004.
Find full textUnited States. National Aeronautics and Space Administration., ed. Current Lewis turbomachinery research: Building on our legacy of excellence. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. Towards a comprehensive computational simulation system for turbomachinery. [Washington, DC: National Aeronautics and Space Administration, 1994.
Find full text1913-, Hawthorne William Sir, and United States. National Aeronautics and Space Administration., eds. Three-dimensional flow in radial turbomachinery and its impact on design. Cambridge, MA: Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1993.
Find full textThree-dimensional flow in radial turbomachinery and its impact on design. Cambridge, MA: Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1993.
Find full textThree-dimensional flow in radial turbomachinery and its impact on design. Cambridge, MA: Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1993.
Find full textP, Van Hooser Katherine, and United States. National Aeronautics and Space Administration., eds. A general fluid system simulation program to model secondary flows in turbomachinery. [Washington, D.C: National Aeronautics and Space Administration, 1995.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Three-Dimensional Flow in Radial Turbomachinery and Its Impact on Design. Independently Published, 2019.
Find full textUnited States. National Aeronautics and Space Administration., ed. An interactive grid generation procedure for axial and radial flow turbomachinery. [Washington, DC?]: National Aeronautics and Space Administration, 1990.
Find full textD, Montgomery Matthew, Kousen Kenneth A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
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