Books on the topic 'Compressors stage'
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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.
Find full textHill, Philip G. An educational introduction to transonic compressor stage design principles. Warrendale, Pa: Society of Automotive Engineers, 1993.
Find full textHaynes, Joel M. Active control of rotating stall in a three-stage axial compressor. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1993.
Find full textWilde, Geoffrey. Flow matching of the stages of axial compressors. Derby: Rolls-Royce Heritage Trust, 1999.
Find full textO'Brien, Joseph Morton. Transonic Compressor Test Rig rebuild and initial results with the Sanger stage. Monterey, Calif: Naval Postgraduate School, 2000.
Find full textNewman, 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.
Find full textChmielniak, Tadeusz. SYMKOM'99: International conference compressor & turbine stage flow path theory, experiment & user verification. Łódź: Politechnika Łʹodzka, Instytut Maszn Przeoływowych, 1999.
Find full textSwansson, N. S. Investigation of blade vibration T55-L-11C compressor stages 1 and 2. Melbourne, Victoria: Aeronautical Research Laboratories, 1985.
Find full textUnited 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.
Find full textDesign 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.
Find full textDesign 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.
Find full textAnalysis of the Sensitivity of Multi-Stage Axial Compressors to Fouling at Various Stages. Storming Media, 2002.
Find full textDesign of a low aspect ratio transonic compressor stage using CFD techniques. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Find full textSimulated dynamic response of a multi-stage compressor with variable molecular weight flow medium. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCenter, Langley Research, ed. Simulated dynamic response of a multi-stage compressor with variable molecular weight flow medium. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textDynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Find full textPreliminary Design Code for an Axial Stage Compressor. Storming Media, 2001.
Find full textL, Gundy-Burlet Karen, and Ames Research Center, eds. Temporally and spatially resolved flow in a two-stage axial compressor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textL, Gundy-Burlet Karen, and Ames Research Center, eds. Temporally and spatially resolved flow in a two-stage axial compressor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textOptimizing the Efficiency of a Multi-Stage Axial-Flow Compressor: An Application of Stage-Wise Optimization. Storming Media, 1998.
Find full textTransonic Compressor Test Rig Rebuild and Initial Results with the Sanger Stage. Storming Media, 2000.
Find full textDimension determination of precursive stall events in a single stage high speed compressor. [Washington, DC]: National Aeronautics and Space Administration, 1996.
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 textFacility, Dryden Flight Research, ed. The effect of compressor seventh-stage bleed air extraction on performance of the F100-PW-220 afterburning turbofan engine. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1991.
Find full textBayly, Brian. Chemical Change in Deforming Materials. Oxford University Press, 1993. http://dx.doi.org/10.1093/oso/9780195067644.001.0001.
Full textField, John. Therapeutic strategies in managing cardiac arrest. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780199600830.003.0064.
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