Books on the topic '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., and 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, and 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, and 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, and 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, and 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, and 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, and 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, and 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, and 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., and 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, and 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, and 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., and 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, and 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.