Books on the topic 'Axial flow compressors. Compressors. Aerodynamics'

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.

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

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.

Haynes, Joel M. Active control of rotating stall in a three-stage axial compressor. 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.

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

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.

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.

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.

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.

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.

Newman, Frederick A. Experimental vibration damping characteristics of the third-stage rotor of a three-stage transonic axial-flow compressor. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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

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

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

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

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

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

Propulsion and Energetics Panel Specialists' Meeting (68th 1986 Munich, Germany). Engine response to distorted inflow conditions: Papers presented at the Propulsion and Energetics 68th(A) Specialists' Meeting, held in Munich, Germany, 8-9 September 1986. Neuilly-sur-Seine, France: AGARD, 1987.

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

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.

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.

Compressor Instability with Integral Methods. Springer, 2007.

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

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.

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

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.

United States. National Aeronautics and Space Administration., ed. Experimental determination of aerodynamic damping in a three-syage transonic axial-flow compressor. [Washington, DC: National Aeronautics and Space Administration, 1988.

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.

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.

1939-, Okiishi T. H., and United States. National Aeronautics and Space Administration., eds. Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance. [Washington, DC]: National Aeronautics and Space Administration, 1996.

R, Wood Jerry, Wasserbauer Charles A, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. NASA low-speed centrifugal compressor for 3-D viscous code assessment and fundamental flow physics research. [Washington, DC]: National Aeronautics and Space Administration, 1991.

R, Wood Jerry, Wasserbauer Charles A, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. NASA low-speed centrifugal compressor for 3-D viscous code assessment and fundamental flow physics research. [Washington, DC]: National Aeronautics and Space Administration, 1991.

R, Wood Jerry, Wasserbauer Charles A, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. NASA low-speed centrifugal compressor for 3-D viscous code assessment and fundamental flow physics research. [Washington, DC]: National Aeronautics and Space Administration, 1991.

M, Greitzer Edward, and Lewis Research Center, eds. 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.

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

Gresh, M. Theodore. Compressor Performance: Selection, Operation, and Testing of Axial and Centrifugal Compressors. Butterworth-Heinemann, 1990.

Method for the determination of the three-dimensional aerodynamic field of a rotor-stator combination in compressible flow. [Washington, DC]: National Aeronautics and Space Administration, 1987.

Unsteady flows in aeropropulsion: Presented at 1994 International Mechanical Engineering Congress and Exposition, Chicago, Illinois, November 6-11, 1994. New York, N.Y: American Society of Mechanical Engineers, 1994.