Books on the topic 'Finite speed of propagation'

Pommier, Sylvie, Anthony Gravouil, Alain Combescure, and Nicolas Moës. Extended Finite Element Method for Crack Propagation. Hoboken, NJ USA: John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118622650.

T, McDaniel S., ed. Ocean acoustic propagation by finite difference methods. Oxford: Pergamon Press, 1988.

Zingg, D. W. An optimized finite-difference scheme for wave propagation problems. Washington, D. C: AIAA, 1993.

E, Turkel, and Institute for Computer Applications in Science and Engineering., eds. Accurate finite difference methods for time-harmonic wave propagation. Hampton, Va: Institute for COmputer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Jurgens, Henry Martin. High-accuracy finite-difference schemes for linear wave propagation. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1997.

Lewicki, David G. Effect of speed (centrifugal load) on gear crack propagation direction. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Epstein, Eric Martin. A comparison of finite-difference schemes for linear wave propagation problems. [Toronto, Ont.]: University of Toronto, Graduate Dept. of Aerospace Science and Engineering, 1995.

Epstein, Eric Martin. A comparison of finite-difference schemes for linear wave propagation problems. Ottawa: National Library of Canada, 1994.

LeVeque, Randall J. High resolution finite volume methods on arbitrary grids via wave propagation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

H, Hung H., ed. Wave propagation for train-induced vibrations: A finite/infinite element approach. Hackensack, NJ: World Scientific, 2009.

LeVeque, Randall J. High resolution finite volume methods on arbitrary grids via wave propagation. Hampton, Va: ICASE, 1987.

University of Wales. Institute for Numerical Methods in Engineering. and Langley Research Center. Aerothermal Loads Branch., eds. Finite element methods of analysis for high speed viscous flows. Hampton, Va: Aerothermal Loads Branch, Loads and Aeroelasticity Division, NASA Langley Research Center, 1987.

Center, Langley Research, ed. Preliminary structural sizing of a Mach 3.0 high-speed civil transport model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Marburg, Steffen, and Bodo Nolte, eds. Computational Acoustics of Noise Propagation in Fluids - Finite and Boundary Element Methods. Berlin, Heidelberg: Springer Berlin Heidelberg, 2008. http://dx.doi.org/10.1007/978-3-540-77448-8.

Steffen, Marburg, and Nolte Bodo, eds. Computational acoustics of noise propagation in fluids: Finite and boundary element methods. Berlin: Springer, 2008.

Baumeister, Kenneth J. A finite element model for wave propagation in an inhomogeneous [i.e. inhomogenous]. [Washington, DC]: National Aeronautics and Space Administration, 1987.

James, William L. Effect of transverse moisture content gradients on the longitudinal propagation of sound in wood. Madison, WI: U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1986.

A, McCurdy David, and Langley Research Center, eds. High-speed research: 1994 Sonic Boom Workshop : atmospheric propagation and acceptability studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

A, McCurdy David, and Langley Research Center, eds. High-speed research: 1994 Sonic Boom Workshop : atmospheric propagation and acceptability studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Laboratory, Construction Engineering Research, ed. A finite difference numerical model for the propagation of finite amplitude acoustical blast waves outdoors over hard and porous surfaces. Champaign, Ill: US Army Corps of Engineers, Construction Engineering Research Laboratory, 1991.

Janaswamy, Ramakrishna. Efficient parabolic equation solution of radiowave propagation in an inhomogeneous atmosphere and over irregular terrain: Formulation. Monterey, Calif: Naval Postgraduate School, 1994.

Janaswamy, Ramakrishna. Efficient parabolic equation solution of radiowave propagation in an inhomogeneous atmosphere and over irregular terrain: Formulation. Monterey, Calif: Naval Postgraduate School, 1994.

Schaffers, Ir. Paulus, J. J. Wave propagation in electrically conducting mixtures of inhomogeneities in liquids. Aachen: Shaker, 1993.

Lewicki, David G. Effect of rim thickness on gear crack propagation path. [Washington, DC: National Aeronautics and Space Administration, 1996.

Lewicki, David G. Effect of rim thickness on gear crack propagation path. [Washington, DC: National Aeronautics and Space Administration, 1996.

Gopalakrishnan, S. Spectral finite element method: Wave propagation, diagnostics and control in anisotropic and inhomogenous structures. London: Springer, 2008.

M, Wicks T., Eversman Walter, and United States. National Aeronautics and Space Administration., eds. Fundamental investigations of the finite element solutions for acoustic propagation in ducts: Final report. [Washington, DC: National Aeronautics and Space Administration, 1986.

Gopalakrishnan, S. Spectral finite element method: Wave propagation, diagnostics and control in anisotropic and inhomogenous structures. London: Springer, 2008.

Gopalakrishnan, S. Spectral finite element method: Wave propagation, diagnostics and control in anisotropic and inhomogenous structures. London: Springer, 2008.

Chatterjee, A. Investigation of finite element-ABC methods for electromagnetic field simulation. Ann Arbor, Mich: University of Michigan, Radiation Laboratory, Dept. of Electrical Engineering and Computer Science, 1994.

Janaswamy, Ramakrishna. Application of the measured equation of invariance to wave propagation over irregular, inhomogeneous terrain. Monterey, Calif: Naval Postgraduate School, 1993.

R, Watson Willie, and Langley Research Center, eds. A finite element propagation model for extracting normal incidence impedance in nonprogressive acoustic wave fields. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Baumeister, Kenneth J. Preconditioning the helmholtz equation for rigid ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Hsing-jen, Chang, and Langley Research Center, eds. H-P adaptive methods for finite element analysis of aerothermal loads in high-speed flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Xingren, Zhang, and Langley Research Center, eds. H-P adaptive methods for finite element analysis of aerothermal loads in high-speed flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Hsing-jen, Chang, and Langley Research Center, eds. H-P adaptive methods for finite element analysis of aerothermal loads in high-speed flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Zingg, D. W. A review of high-order and optimized finite-difference methods for simulating linear wave phenomena. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1996.

Zingg, D. W. A review of high-order and optimized finite-difference methods for simulating linear wave phenomena. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1996.

Zingg, D. W. A review of high-order and optimized finite-difference methods for simulating linear wave phenomena. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1996.

United States. National Aeronautics and Space Administration., ed. Parametric study on laminar flow for finite wings at supersonic speeds. [Washington, DC]: National Aeronautics and Space Administration, 1994.

J, Ehernberger L., Whitmore Stephen A, and Dryden Flight Research Facility, eds. Preliminary airborne measurements for the SR-71 sonic boom propagation experiment. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1995.

J, Ehernberger L., Whitmore Stephen A, and Dryden Flight Research Facility, eds. Preliminary airborne measurements for the SR-71 sonic boom propagation experiment. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1995.

Baumeister, Kenneth J. Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow. [Washington, D.C: National Aeronautics and Space Administration, 1996.

Baumeister, Kenneth J. Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow. [Washington, D.C: National Aeronautics and Space Administration, 1996.

G, Dávila C., and Ambur D. R, eds. Numerical simulation of delamination growth in composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

Jun, Fang, Kurbatskii Konstantin A, and United States. National Aeronautics and Space Administration., eds. Inhomogeneous radiation boundary conditions simulating incoming acoustic waves for computational aeroacoustics. [Washington, DC: National Aeronautics and Space Administration, 1996.

Camanho, P. P. Numerical simulation of delamination growth in composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

United States. National Aeronautics and Space Administration., ed. High speed civil transport: Sonic boom softening and aerodynamic optimization. San Jose, CA: MCAT Institute, 1994.

Koning, A. V. de. Finite element analyses of stable crack growth in thin sheet material. Amsterdam: National Aerospace Laboratory, 1985.

Piras, Gabriel. Dynamic finite-element analysis of a planar high-speed, high-precision parallel manipulator with flexible links. Ottawa: National Library of Canada, 2003.