Livres sur le sujet « Unsteady mode »
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Vest, Michael S. Unsteady aerodynamic model of flapping wings. Washington, D. C : AIAA, 1995.
Webb, J. C. On the nonlinear stability of viscous modes within the Rayleigh problem of an infinite flat plate. Hampton, Va : Institute for Computer Applications in Science and Engineering, 1994.
Winfield, James Frederick. A three-dimensional unsteady aerodynamic model with applications to flapping-wing propulsion. [Downsview, Ont.] : University of Toronto, Department of Aerospace Science and Engineering, 1990.
Winfield, James Frederick. A three-dimensional unsteady aerodynamic model with applications to flapping-wing propulsion. Ottawa : National Library of Canada, 1990.
Westland, J. Clebsch variable model for unsteady inviscid transonic flow with strong shock waves. Amsterdam : National Aerospace Laboratory, 1993.
Boer, R. G. den. Revised results of the unsteady transonic pressure measurements on the LANN model. Amsterdam : National Aerospace Laboratory, 1989.
DeLong, Lewis L. Computer program HYDRAUX : A model for simulating one-dimensional, unsteady, open-channel flow. Reston, Va : Dept. of the Interior, U.S. Geological Survey, 1989.
Berry, John D. Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1997.
Hosseini, Seyed Mahmood. Development of an unsteady non-linear model for flow through coarse porous media. Guelph, Ont : University of Guelph, 1997.
Ishii, Audrey L. Verification of a one-dimensional, unsteady-flow model for the Fox River in Illinois. Washington, DC : U.S. G.P.O., 1996.
Menzies, Margaret Anne. Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : A multidisciplinary problem. [Norfolk, VA : Old Dominion University, 1996.
Turner, Mary J. Implementation and verification of a one-dimensional, unsteady-flow model for Spring Brook near Warrenville, Illinois. Washington : U.S. G.P.O., 1996.
Wiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. Boulder, Colo : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Wiele, Stephen Mark. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. Boulder, Colo : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Wiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. Boulder, Colo : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Wiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. Boulder, Colo : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Wiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. Boulder, Colo : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Wiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. Boulder, Colo : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Wiele, Stephen Mark. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. Boulder, Colo : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Wiele, Stephen M. Modifications to a one-dimensional model of unsteady flow in the Colorado River through the Grand Canyon, Arizona. Boulder, Colo : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Franz, Delbert D. Full equations utilities (FEQUTL) model for the approximation of hydraulic characteristics of open channels and control structures during unsteady flow. Urbana, Ill : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Zdunich, Patrick. A discrete vortex model of unsteady separated flow about a thin airfoil for application to hovering flapping-wing flight. [Downsview, Ont.] : University of Toronto, Institute for Aerospace Studies, 2002.
Zdunich, Patrick. A discrete vortex model of unsteady separated flow about a thin airfoil for application to hovering flapping-wing flight. Ottawa : National Library of Canada, 2002.
Laenen, Antonius. Simulation of three lahars in the Mount St. Helens area, Washington using a one-dimensional, unsteady-state streamflow model. Portland, Or : Dept. of the Interior, U.S. Geological Survey, 1988.
Franz, 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. Mountain View, Calif : U.S. Dept. of the Interior, U.S. Geological Survey, 1997.
Makhmudov, Ilkhom Ernazarovich. UNSTEADY WATER MOVEMENT IN THE CANALS DUE TO THE PUMPING STATIONS OPERATION MODE. RS Global S. z O.O., 2022. http://dx.doi.org/10.31435/rsglobal/045.
United States. National Aeronautics and Space Administration., dir. A numerical model of unsteady, subsonic aeroelastic behavior. [Washington, D.C : National Aeronautics and Space Administration, 1987.
P, Woodward Richard, et United States. National Aeronautics and Space Administration., dir. Unsteady blade pressure measurements on a model counterrotation propeller. [Washington, DC] : National Aeronautics and Space Administration, 1989.
G, Jones Michael, Thurlow Ernie M et United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. Unsteady pressure loads in a generic high-speed engine model. [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
G, Jones Michael, Thurlow Ernie M et United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. Unsteady pressure loads in a generic high-speed engine model. [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
United States. National Aeronautics and Space Administration., dir. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC] : National Aeronautics and Space Administration, 1992.
Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC] : National Aeronautics and Space Administration, 1992.
United States. National Aeronautics and Space Administration., dir. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC] : National Aeronautics and Space Administration, 1992.
A, Rivera José, et Langley Research Center, dir. NACA0012 benchmark model using experimental flutter results with unsteady pressure distributions. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1992.
E, Paxson Daniel, et Lewis Research Center, dir. A simplified model for the investigation of acoustically driven combustion instabilities. [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998.
R, Mankbadi R., et United States. National Aeronautics and Space Administration., dir. A rapid-distortion-theory turbulence model for developed unsteady wall-bounded flow. [Washington, DC] : National Aeronautics and Space Administration, 1993.
A rapid-distortion-theory turbulence model for developed unsteady wall-bounded flow. [Washington, DC] : National Aeronautics and Space Administration, 1993.
A rapid-distortion-theory turbulence model for developed unsteady wall-bounded flow. [Washington, DC] : National Aeronautics and Space Administration, 1993.
Center, Langley Research, et U.S. Army Aviation and Troop Command., dir. Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1997.
A, Rivera José, et Langley Research Center, dir. Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1991.
Nicolas, Spitz, et NASA Glenn Research Center, dir. Predicting modes of the unsteady vorticity field near the trailing edge of a blade. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 2003.
Nicolas, Spitz, et NASA Glenn Research Center, dir. Predicting modes of the unsteady vorticity field near the trailing edge of a blade. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 2003.
J, Heidelberg Laurence, Envia Edmane et NASA Glenn Research Center, dir. Coupling of low speed fan stator vane unsteady pressures to duct modes : Measured versus predicted. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 1999.
V, Kaza K. R., et United States. National Aeronautics and Space Administration., dir. Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter. [Washington, DC] : National Aeronautics and Space Administration, 1992.
Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter. [Washington, DC] : National Aeronautics and Space Administration, 1992.
V, Kaza K. R., et United States. National Aeronautics and Space Administration., dir. Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter. [Washington, DC] : National Aeronautics and Space Administration, 1992.
Tuncer, Cebeci, et United States. National Aeronautics and Space Administration., dir. A General method for unsteady stagnation region heat transfer and results for model turbine flows. [Washington, DC] : National Aeronautics and Space Administration, 1987.
J, Heidelberg Laurence, Envia Edmane et NASA Glenn Research Center, dir. Coupling of low speed fan stator vane unsteady pressures to duct modes : Measured versus predicted. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 1999.
United States. National Aeronautics and Space Administration., dir. A new unsteady mixing model to predict NOx production during rapid mixing in a dual-stage combustor. [Washington, DC] : National Aeronautics and Space Administration, 1992.
A new unsteady mixing model to predict NOx production during rapid mixing in a dual-stage combustor. [Washington, DC] : National Aeronautics and Space Administration, 1992.