Books on the topic 'Design of axial compressors'

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

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.

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

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

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.

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.

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

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

Moore, F. K. A theory of post-stall transients in multistage axial compression systems. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Blading design for axial turbomachines. Neuilly sur Seine, France: AGARD, 1989.

Gresh, M. Theodore. Compressor performance: Selection,operation, and testing of axial and centrifugal compressors. Stoneham, Mass: Butterworth-Heinemann, 1991.

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

Compressor performance: Selection, operation, and testing of axial and centrifugal compressors. Boston: Butterworth-Heinemann, 1991.

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

Braembussche, René Van den. Design and Analysis of Centrifugal Compressors. Chichester, UK: John Wiley & Sons, Ltd, 2019. http://dx.doi.org/10.1002/9781119424086.

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.

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

Institute of Marine Engineering, Science and Technology., ed. Design and operation of marine air compressors. London: IMarEst, 2005.

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

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.

Lüdtke, Klaus H. Process Centrifugal Compressors: Basics, Function, Operation, Design, Application. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004.

Whitfield, A. Design of radial turbomachines. Harlow, Essex, England: Longman Scientific & Technical, 1990.

Simmons, Peter. Guide to European compressors and their applications: The complete practical reference guide to compressors design, operation and applications. Bury St Edmunds: Professional Engineering Pub., 2003.

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

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

Japikse, David. Centrifugal compressor design and performance. Wilder, Vt: Concepts ETI, 1996.

Centrifugal compressor design and performance. Wilder, Vt: Concepts ETI, 1988.

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

Centrifugal compressors: A strategy for aerodynamic design and analysis. New York: ASME Press, 2000.

Gieras, Jacek F. Axial flux permanent magnet brushless machines. 2nd ed. [New York]: Springer, 2008.

Gieras, Jacek F. Axial flux permanent magnet brushless machines. Dordrecht: Kluwer Academic, 2003.

Hill, Philip G. An educational introduction to transonic compressor stage design principles. Warrendale, Pa: Society of Automotive Engineers, 1993.

Stepanoff, Alexey J. Centrifugal and axial flow pumps: Theory, design, and application. Malabar, Fla: Krieger Pub. Co., 1993.

Ball, Calvin L. Advanced technology's impact on compressor design and development: A perspective. Warrendale, PA: Society of Automotive Engineers, 1989.

Sapiro, Leon. Aerodynamic performance of centrifugal compressors for gas and oil applications. New York: ASME, 2007.

Aizpuru, Jesús Landa. Pistones para motores térmicos y compresores alternativos: Diseño, cálculo, simulación y ensayos. Vitoria: Servicio Editorial, Universidad del País Vasco, 2014.

Tam, C. H. Design and development of axial-field air-cored brushless DC motors. [s.l.]: typescript, 1985.

Turbine aerodynamics: Axial-flow and radial-inflow turbine design and analysis. New York: ASME Press, 2006.

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.

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.

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.

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

Preliminary Design Code for an Axial Stage Compressor. Storming Media, 2001.

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.

M, Lavelle Thomas, and United States. National Aeronautics and Space Administration., eds. Enhanced capabilities and modified users manual for axial-flow compressor conceptual design code CSPAN. [Washington, DC]: National Aeronautics and Space Administration, 1995.