Books on the topic 'Gas flow in axial compressors'

Buisine, D. Modelisation du grand decrochage dans les compresseurs axiaux. Rhode Saint Genese, Belgium: Von Karman Institute for Fluid Dynamics, 1988.

Wilde, Geoffrey. Flow matching of the stages of axial compressors. Derby: Rolls-Royce Heritage Trust, 1999.

Design of highly loaded axial-flow fans and compressors. White River Junction, Vt: Concepts ETI, 2000.

Cyrus, Václav. Secondary flow in axial compressors and its effect on aerodynamic characteristics. Praha: National Research Institute for Machine Design, Praha-Běchovice, 1988.

Steinke, Ronald J. Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages. Cleveland, Ohio: Lewis Research Center, 1986.

Paduano, James D. Active control of rotating stall in axial compressors. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1992.

Axial-flow compressors: A strategy for aerodynamic design and analysis. New York: ASME Press, 2003.

Wennerstrom, Arthur J. Low aspect ratio axial flow compressors: Why and what it means. Warrendale, PA: Society of Automotive Engineers, 1986.

Time-marching: A step-by-step guide to a flow solver. Aldershot, Hants., England: Ashgate, 1997.

Haynes, Joel M. Active control of rotating stall in a three-stage axial compressor. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1993.

Shahrokhani, Mohamad. Wall boundary layers in cascades of axial flow compressors with and without secondary flow effects. Birmingham: University of Birmingham, 1990.

Gysling, Daniel L. Dynamic control of rotating stall in axial flow compressors using aeromechanical feedback. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1993.

Riggle, Peter. Investigation of axial positioning for flexural compressors: Final technical report. Richland, WA: Tri-Cities University Center, University of Washington, 1991.

Nichols, Jason C. A three-dimensional multi-block Newton-Krylov flow solver for the Euler equations. [Downsview, Ont: University of Toronto, Institute for Aerospace Studies], 2004.

Arasu, A. Valan. Turbo machines. New Delhi: Vikas Publishing House, 2008.

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

Jadayel, Oussama Chafic. Experimental investigation and theoretical treatment of the role of turbulent stresses in axial flow compressors. Birmingham: University of Birmingham, 1989.

Schmidt, James F. Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors: User's manual. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Ng, Y. K. Eddie. Compressor instability with integral methods. Berlin: Springer, 2007.

Chung-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.

Chung-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.

Murthy, S. N. B. The WINCOF-I code: Detailed description. [Washington, D.C.]: National Aeronautics and Space Administration, 1993.

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

Aungier, Ronald H. Axial-Flow Compressors. ASME Press, 2003. http://dx.doi.org/10.1115/1.801926.

Escudier, Marcel. Introduction to Engineering Fluid Mechanics. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.001.0001.

E, Breugelmans F. A., and Von Karman Institute for Fluid Dynamics., eds. Axial flow compressors: January 27-30 1992. Rhode Saint Genèse, Belgium: Von Karman Institute for Fluid Dynamics, 1992.

Unsteady flow field in a multistage axial flow compressor. University Park, PA: Center for Gas Turbine and Power, The Pennsylvania State University ; [Cleveland, Ohio, 1997.

Stepped Tip Gap Effects on a Transonic Axial-Flow Compressor Rotor. Storming Media, 1997.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

United States. National Aeronautics and Space Administration., ed. Users manual for updated computer code for axial-flow compressor conceptual design. [Washington, DC: National Aeronautics and Space Administration, 1992.

Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Japiske, David. Design of Highly Loaded Axial-Flow Fans and Compressors. Concepts Eti, 2001.

Aungier, Ronald H. Axial-Flow Compressors: A Strategy for Aerodynamic Design and Analysis. American Society of Mechanical Engineers, 2003.

Parker, Philip M. The 2007-2012 World Outlook for New Stationary Centrifugal and Axial Gas Compressors Excluding Natural Gas Compressors. ICON Group International, Inc., 2006.

The 2006-2011 World Outlook for New Stationary Centrifugal and Axial Gas Compressors Excluding Natural Gas Compressors. Icon Group International, Inc., 2005.

Application of modified loss and deviation correlations to transonic axial compressors. Neuilly sur Seine, France: AGARD, 1987.

Axial Flow Fans and Compressors: Aerodynamic Design and Performance (Cranfield Series on Turbomachinery Technology). Ashgate Publishing, 1997.

United States. National Aeronautics and Space Administration., ed. Blockage development in a transonic, axial compressor rotor. [Washington, D.C: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. Blockage development in a transonic, axial compressor rotor. [Washington, D.C: National Aeronautics and Space Administration, 1997.

Nichols, Jason C. A three-dimensional multi-block Newton-Krylov flow solver for the Euler equations. 2004.

Parker, Philip M. The 2007-2012 World Outlook for New Stationary Centrifugal and Axial Natural Gas Compressors. ICON Group International, Inc., 2006.

The 2006-2011 World Outlook for New Stationary Centrifugal and Axial Natural Gas Compressors. Icon Group International, Inc., 2005.

United States. National Aeronautics and Space Administration., ed. Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors: User's manual. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors: User's manual. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Compressor Instability with Integral Methods. Springer, 2007.

Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor. [Washington, DC]: National Aeronautics and Space Administration, 1995.

L, Celestina Mark, and United States. National Aeronautics and Space Administration., eds. Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor. [Washington, DC]: National Aeronautics and Space Administration, 1995.

A, Clark David, Wood Jerry R, United States. Army Aviation Research and Technology Activity. Propulsion Directorate., and Lewis Research Center, eds. Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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.