Libros sobre el tema "Unsteady computations"

Shankar, Vijaya. Unsteady full potential computations for complex configurations. New York: AIAA, 1987.

United States. National Aeronautics and Space Administration., ed. Long time behavior of unsteady flow computations. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Roe, P. L. Remote boundary conditions for unsteady multidimensional aerodynamic computations. Hampton, Va: ICASE, 1986.

Roe, P. L. Remote boundary conditions for unsteady multidimensional aerodynamic computations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Ide, Hiroshi. Unsteady full potential aeroelastic computations for flexible configurations. New York: AIAA, 1987.

Rango, Stan De. Implicit navier-stokes computations of unsteady flows using subiteration methods. Ottawa: National Library of Canada, 1996.

Center, Ames Research, ed. Computations of unsteady multistage compressor flows in a workstation environment. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

V, Kaza K. R. y United States. National Aeronautics and Space Administration., eds. A semianalytical technique for sensitivity analysis of unsteady aerodynamic computations. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Rango, Stan De. Implicit navier-stokes computations of unsteady flows using subiteration methods. [Toronto]: Dept. of Aerospace Science and Engineering, University of Toronto, 1996.

Nakamichi, Jiro. Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing. Tokyo: National Aerospace Laboratory, 1988.

A, Willis Edward y United States. National Aeronautics and Space Administration., eds. Analysis of rotary engine combustion processes based on unsteady, three-dimensional computations. [Washington, D.C.]: NASA, 1990.

United States. National Aeronautics and Space Administration., ed. Steady and unsteady three-dimensional transonic flow computations by integral equation method: Final technical report. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Steady and unsteady three-dimensional transonic flow computations by integral equation method: Final technical report. [Washington, DC: National Aeronautics and Space Administration, 1994.

D, Modiano, Colella P y United States. National Aeronautics and Space Administration., eds. Computations of unsteady viscous compressible flows using adaptive mesh refinement in curvilinear body-fitted grid systems. [Washington, DC]: National Aeronautics and Space Administration, 1994.

D, Modiano, Colella P y United States. National Aeronautics and Space Administration., eds. Computations of unsteady viscous compressible flows using adaptive mesh refinement in curvilinear body-fitted grid systems. [Washington, DC]: National Aeronautics and Space Administration, 1994.

D, Freund Donald y United States. National Aeronautics and Space Administration., eds. Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations: Final technical report. [Washington, DC: National Aeronautics and Space Administration, 1998.

Tucker, Paul G. Computation of Unsteady Internal Flows. Boston, MA: Springer US, 2001. http://dx.doi.org/10.1007/978-1-4615-1439-8.

Obayashi, Shigeru. Progress in computational unsteady aerodynamics. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Tucker, P. G. Unsteady Computational Fluid Dynamics in Aeronautics. Dordrecht: Springer Netherlands, 2014. http://dx.doi.org/10.1007/978-94-007-7049-2.

Edwards, John W. Computational methods for unsteady transonic flows. New York: AIAA, 1987.

United States. National Aeronautics and Space Administration., ed. Unsteady jet flow computation towards noise prediction. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Basco, David R. Computation of rapidly varied unsteady, free-surface flow. Reston, Va: Dept. of the Interior, U.S. Geological Survey, 1987.

Venkatakrishnan, V. Computation of unsteady transonic flows over moving airfoils. Princeton, N.J: Princeton University, 1987.

Krishnan, Radhakrishnan, Zhou Ruhai y NASA Glenn Research Center, eds. Computation of steady and unsteady laminar flames: Theory. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

United States. National Aeronautics and Space Administration., ed. Non-linear unsteady wing theory. [Washington, DC: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., ed. Non-linear unsteady wing theory. [Washington, DC: National Aeronautics and Space Administration, 1987.

Edwards, John W. Assessment of computational prediction of tail buffeting. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Davis, Sanford S. Computation of the unsteady facilitated transport of oxygen in hemoglobin. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Computation of unsteady internal flows: Fundamental methods with case studies. Norwell, Mass: Kluwer Academic Publishers, 2001.

Tucker, Paul G. Computation of Unsteady Internal Flows: Fundamental Methods with Case Studies. Boston, MA: Springer US, 2001.

Waldman, W. An improved computational procedure for the unsteady doublet lattice method. Melbourne, Australia: Aeronautical Research Laboratories, 1986.

P, Guruswamy Guru y Ames Research Center, eds. Computational unsteady transonic aerodynamics and aeroelasticity about airfoils and wings. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Gordon, David R. Computational unsteady flow dynamics: Oscillating flow about a circular cylinder. Monterey, Calif: Naval Postgraduate School, 1991.

R, Quackenbush Todd y Langley Research Center, eds. Computational analysis of high resolution unsteady airloads for rotor aeroacoustics. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Dimitri, Mavriplis y Institute for Computer Applications in Science and Engineering., eds. Implicit method for the computation of unsteady flows on unstructured grids. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

N, Duque Earl P. y United States. National Aeronautics and Space Administration., eds. Helicopter rotor blade computation in unsteady flows using moving overset grids. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.

Dimitri, Mavriplis y Institute for Computer Applications in Science and Engineering., eds. Implicit method for the computation of unsteady flows on unstructured grids. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

T, Batina John, Yang T. Y y Langley Research Center, eds. Spatial adaption procedures on unstructured meshes for accurate unsteady aerodynamic flow computation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Wilson, Gregory Jon. Computation of steady and unsteady shock-induced combustion over hypervelocity blunt bodies. Stanford, Conn: Stanford University, 1992.

F, Clarke J. Numerical computation of two-dimensional unsteady detonation waves in high energy solids. Cranfield, Bedford, England: College of Aeronautics, Cranfield Institute of Technology, 1990.

Janetzke, David C. Efficient computation of aerodynamic influence coefficients for aeroelastic analysis on a transputer network. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Sussman, Myles A. A computational study of unsteady shock induced combustion of hydrogen-air mixtures. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.

Ekaterinaris, John A. Computation of separated and unsteady flows with one- and two-equation turbulence models. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.

1945-, Sharma Om P. y United States. National Aeronautics and Space Administration., eds. Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

Banerjee, I. CFD simulation of flow through single and multi vane spiral pump for low pressure application using moving node unsteady computation. Mumbai: Bhabha Atomic Research Centre, 2010.

Yungster, S. Simulation of unsteady hypersonic combustion around projectiles in an expansion tube. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Center, Langley Research, ed. Unsteady transonic flow calculations for wing-fuselage configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

United States. National Aeronautics and Space Administration., ed. Visualization of unsteady computational fluid dynamics: Final technical report for grant #NAG2-884. [Washington, DC: National Aeronautics and Space Administration, 1997.

Woodrow, Whitlow y Langley Research Center, eds. Development of computational methods for unsteady aerodynamics at the NASA Langley Research Center. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

United States. National Aeronautics and Space Administration., ed. Visualization of unsteady computational fluid dynamics: Final technical report for grant #NAG2-884. Cambridge, MA: Computational Aerospace Sciences Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1994.