Books on the topic 'Unsteady mode'
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United States. National Aeronautics and Space Administration., ed. A numerical model of unsteady, subsonic aeroelastic behavior. National Aeronautics and Space Administration, 1987.
Find full textP, Woodward Richard, and United States. National Aeronautics and Space Administration., eds. Unsteady blade pressure measurements on a model counterrotation propeller. National Aeronautics and Space Administration, 1989.
Find full textWebb, J. C. On the nonlinear stability of viscous modes within the Rayleigh problem of an infinite flat plate. Institute for Computer Applications in Science and Engineering, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. National Aeronautics and Space Administration, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. National Aeronautics and Space Administration, 1992.
Find full textWinfield, James Frederick. A three-dimensional unsteady aerodynamic model with applications to flapping-wing propulsion. University of Toronto, Department of Aerospace Science and Engineering, 1990.
Find full textG, Jones Michael, Thurlow Ernie M, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Unsteady pressure loads in a generic high-speed engine model. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Find full textG, Jones Michael, Thurlow Ernie M, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Unsteady pressure loads in a generic high-speed engine model. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Find full textE, Paxson Daniel, and Lewis Research Center, eds. A simplified model for the investigation of acoustically driven combustion instabilities. National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textA, Rivera José, and Langley Research Center, eds. NACA0012 benchmark model using experimental flutter results with unsteady pressure distributions. National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textBoer, R. G. den. Revised results of the unsteady transonic pressure measurements on the LANN model. National Aerospace Laboratory, 1989.
Find full textWestland, J. Clebsch variable model for unsteady inviscid transonic flow with strong shock waves. National Aerospace Laboratory, 1993.
Find full textWinfield, James Frederick. A three-dimensional unsteady aerodynamic model with applications to flapping-wing propulsion. National Library of Canada, 1990.
Find full textR, Mankbadi R., and United States. National Aeronautics and Space Administration., eds. A rapid-distortion-theory turbulence model for developed unsteady wall-bounded flow. National Aeronautics and Space Administration, 1993.
Find full textBerry, John D. Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textDeLong, Lewis L. Computer program HYDRAUX: A model for simulating one-dimensional, unsteady, open-channel flow. Dept. of the Interior, U.S. Geological Survey, 1989.
Find full textA, Rivera José, and Langley Research Center, eds. Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textHosseini, Seyed Mahmood. Development of an unsteady non-linear model for flow through coarse porous media. University of Guelph, 1997.
Find full textCenter, Langley Research, and U.S. Army Aviation and Troop Command., eds. Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textNicolas, Spitz, and NASA Glenn Research Center, eds. Predicting modes of the unsteady vorticity field near the trailing edge of a blade. National Aeronautics and Space Administration, Glenn Research Center, 2003.
Find full textIshii, Audrey L. Verification of a one-dimensional, unsteady-flow model for the Fox River in Illinois. U.S. G.P.O., 1996.
Find full textNicolas, Spitz, and NASA Glenn Research Center, eds. Predicting modes of the unsteady vorticity field near the trailing edge of a blade. National Aeronautics and Space Administration, Glenn Research Center, 2003.
Find full textTuncer, Cebeci, and United States. National Aeronautics and Space Administration., eds. A General method for unsteady stagnation region heat transfer and results for model turbine flows. National Aeronautics and Space Administration, 1987.
Find full textMenzies, Margaret Anne. Unsteady, transonic flow around delta wings undergoing coupled and natural modes response: A multidisciplinary problem. Old Dominion University, 1996.
Find full textJ, Heidelberg Laurence, Envia Edmane, and NASA Glenn Research Center, eds. Coupling of low speed fan stator vane unsteady pressures to duct modes: Measured versus predicted. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textV, Kaza K. R., and United States. National Aeronautics and Space Administration., eds. Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter. National Aeronautics and Space Administration, 1992.
Find full textJ, Heidelberg Laurence, Envia Edmane, and NASA Glenn Research Center, eds. Coupling of low speed fan stator vane unsteady pressures to duct modes: Measured versus predicted. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textV, Kaza K. R., and United States. National Aeronautics and Space Administration., eds. Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter. National Aeronautics and Space Administration, 1992.
Find full textUnited States. Army. Corps of Engineers., U.S. Army Engineer Waterways Experiment Station., and Environmental Laboratory (U.S. Army Engineer Waterways Experiment Station), eds. CE-QUAL-RIV1: A dynamic, one-dimensional (longitudinal) water quality model for streams : user's manual. U.S. Army Engineer Waterways Experiment Station, 1995.
Find full textTurner, Mary J. Implementation and verification of a one-dimensional, unsteady-flow model for Spring Brook near Warrenville, Illinois. U.S. G.P.O., 1996.
Find full textWiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textWiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textWiele, Stephen Mark. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textWiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textWiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textWiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textWiele, Stephen Mark. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textWiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textR, Otto S., Lilley G. M, and Institute for Computer Applications in Science and Engineering., eds. On the nonlinear stability of viscous modes within the Rayleigh problem on an infinite flat plate. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Find full textFranz, Delbert D. Full equations utilities (FEQUTL) model for the approximation of hydraulic characteristics of open channels and control structures during unsteady flow. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. A new unsteady mixing model to predict NOx production during rapid mixing in a dual-stage combustor. National Aeronautics and Space Administration, 1992.
Find full textJiunn-Chi, Wu, and Lewis Research Center, eds. Studies of unsteady viscous flows using a two-equation model of turbulence: Semi-annual status report for the period January 1 - June 30, 1987. The Center, 1987.
Find full textLaenen, Antonius. Simulation of three lahars in the Mount St. Helens area, Washington using a one-dimensional, unsteady-state streamflow model. Dept. of the Interior, U.S. Geological Survey, 1988.
Find full textZdunich, Patrick. A discrete vortex model of unsteady separated flow about a thin airfoil for application to hovering flapping-wing flight. National Library of Canada, 2002.
Find full textZdunich, Patrick. A discrete vortex model of unsteady separated flow about a thin airfoil for application to hovering flapping-wing flight. University of Toronto, Institute for Aerospace Studies, 2002.
Find full textUnited States. National Aeronautics and Space Administration., ed. System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality: A dissertation ... National Aeronautics and Space Administration, 1997.
Find full textL, Maples Anna, and United States. National Aeronautics and Space Administration., eds. MPS solidification model: Final report, analysis and calculation of macrosegregation in a casting ingot. General Electric Co., Space Systems Division, Huntsville Center Operations, 1985.
Find full textSerikov, Sergey. Impact on impact strength. INFRA-M Academic Publishing LLC., 2024. http://dx.doi.org/10.12737/2161513.
Full textFranz, Delbert D. Full Equations (FEQ) model for the solution of the full, dynamic equations of motion for one-dimensional unsteady flow in open channels and through control structures. U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
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