Libri sul tema "Computation speedup"

Roberts, Leonard. Computation of high speed transport aerodynamics. Stanford, Calif: Stanford University, Dept. of Aeronautics and Astronautics, 1991.

Abolhassani, Jamshid S. Topology and grid adaption for high-speed flow computations. Hampton, Va: Langley Research Center, 1989.

Tauber, Michael E. A review of high-speed, convective, heat-transfer computation methods. Moffett Field, Calif: Ames Research Center, 1989.

Rostand, Philippe. Algebraic turbulence models for the computation of two-dimensional high speed flows using unstructured grids. Hampton, Va: ICASE, 1988.

Gentzsch, Wolfgang. High speed and large scale scientific computing. Amsterdam: IOS Press, 2009.

Gentzsch, Wolfgang. High speed and large scale scientific computing. Amsterdam: IOS Press, 2009.

Thareja, R. R. Applications of an adaptive unstructured solution algorithm to the analysis of high speed flows. Washington, D. C: American Institute of Aeronautics and Astronautics, 1990.

Coirier, William J. Efficient real gas Navier-Stokes computations of high speed flows using an LU scheme. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Taki, Mustafa. Computation of the aerodynamic performance of high-lift aerofoil systems at low-speed and transonic flow conditions. Manchester: UMIST, 1997.

Groth, Clinton P. T. TVD flux-difference split methods for high-speed thermochemical nonequilibrium flows with strong shocks. [Toronto, Ont.]: University of Toronto, Graduate Dept. of Aerospace Science and Engineering, 1993.

Groth, Clinton P. T. TVD flux-difference split methods for high-speed thermochemical equilibrium flows with strong shocks. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 1993.

Bell, J. H. Contraction design for small low-speed wind tunnels. [Washington, DC: National Aeronautics and Space Administration, 1988.

Szuch, John R. Enhancing aeropropulsion research with high-speed interactive computing. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

Walker, J. D. A. Embedded function methods for compressible high speed turbulent flow: Final report. Hampton, Va: NASA Langley Research Center, 1994.

Pope, Stephen B. PDF methods for combustion in high-speed turbulent flows: Second annual technical report. [Washington, D.C: National Aeronautics and Space Administration, 1995.

El-Hady, Nabil M. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. Hampton, Va: Langley Research Center, 1993.

Podleski, Steve D. PARC3D calculations of the F/A-18A HARV inlet vortex generators. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

G, Rehm Ronald, National Institute of Standards and Technology (U.S.) e Building and Fire Research Laboratory (U.S.), a cura di. An efficient large eddy simulation algorithm for computational wind engineering: Application to surface pressure computations on a single building. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.

G, Rehm Ronald, National Institute of Standards and Technology (U.S.) e Building and Fire Research Laboratory (U.S.), a cura di. An efficient large eddy simulation algorithm for computational wind engineering: Application to surface pressure computations on a single building. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.

A review of high-speed, convective, heat-transfer computation methods. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., a cura di. A review of high-speed, convective, heat-transfer computation methods. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Topology and grid adaption for high-speed flow computations. Norfolk, Va: Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1988.

N, Tiwari S., e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., a cura di. Topology and grid adaptation for high-speed flow computations. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Anderson, James A. The Past of the Future of Computation. Oxford University Press, 2018. http://dx.doi.org/10.1093/acprof:oso/9780199357789.003.0001.

Unstructured adaptive mesh computations of rotorcraft high-speed impulsive noise. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1993.

Michael, Garceau, Biswas Rupak e Research Institute for Advanced Computer Science (U.S.), a cura di. Unstructured adaptive mesh computations of rotorcraft high-speed impulsive noise. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1993.

Center, Lewis Research, a cura di. Application of computational fluid dynamics in high speed aeropropulsion. [Cleveland, Ohio: Lewis Research Center, 1991.

(Editor), J. A. Desideri, W. Fitzgibbon (Editor), R. Glowinski (Editor) e J. Periaux (Editor), a cura di. High Speed Flow Fields (Computational Methods in Applied Sciences). John Wiley & Sons Inc, 1999.

Dolatabadi, Ali. A computational analysis of high speed particle-laden flows. 2002.

J, Wilson Gregory, e United States. National Aeronautics and Space Administration., a cura di. Computations of axisymmetric flows in hypersonic shock tubes. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

National Aeronautics and Space Administration (NASA) Staff. Inviscid Computational Study of an X-33 Configuration at Hypersonic Speeds. Independently Published, 2018.

An inviscid computational study of an X-33 configuration at hypersonic speeds. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, a cura di. An inviscid computational study of an X-33 configuration at hypersonic speeds. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

D, Hathaway M., United States. National Aeronautics and Space Administration. e U.S. Army Research Laboratory., a cura di. Experimental and computational results from a large low-speed centrifugal impeller. [Washington, DC]: National Aeronautics and Space Administration, 1993.

D, Hathaway Michael, United States. National Aeronautics and Space Administration. e U.S. Army Research Laboratory., a cura di. Experimental and computational results from a large low-speed centrifugal impeller. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Investigation of parabolic computational techniques for internal high-speed viscous flows. East Hartford, CT: United Technologies Research Center, 1985.

Center, Langley Research, a cura di. Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

A, Wahls Richard, e Langley Research Center, a cura di. Turbulence model comparisons for a high-speed aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Geshi, Masaaki. The Art of High Performance Computing for Computational Science, Vol. 1: Techniques of Speedup and Parallelization for General Purposes. Springer, 2020.

Geshi, Masaaki. The Art of High Performance Computing for Computational Science, Vol. 1: Techniques of Speedup and Parallelization for General Purposes. Springer, 2019.

United States. National Aeronautics and Space Administration., a cura di. High speed civil transport aerodynamic optimization. San Jose, CA: MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., a cura di. High speed civil transport aerodynamic optimization. San Jose, CA: MCAT Institute, 1994.

Center, Langley Research, a cura di. Algebraic turbulence models for the computation of two-dimensional high speed flows using unstructured grids. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

United States. National Aeronautics and Space Administration., a cura di. Efficient real gas Navier-Stokes computations of high speed flows using an LU scheme. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Addition & Subtraction Flashcard Games: 25 Fun Games to Improve Speed and Accuracy in Computation (Flashcard Games). Teaching Resources, 2004.

D, Hathaway Michael, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., a cura di. Experimental and computational investigation of the NASA low-speed centrifugal compressor flow field. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

D, Hathaway Michael, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., a cura di. Experimental and computational investigation of the NASA low-speed centrifugal compressor flow field. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Mesinger, Fedor, Miodrag Rančić e R. James Purser. Numerical Methods in Atmospheric Models. Oxford University Press, 2018. http://dx.doi.org/10.1093/acrefore/9780190228620.013.617.

High-Resolution Methods for Incompressible and Low-Speed Flows (Computational Fluid and Solid Mechanics). Springer, 2004.