Books on the topic 'Potential flow'

1940-, Rahman M., ed. Potential flow of fluids. Southampton: Computational Mechanics Publications, 1995.

Salas, Manuel D. Breakdown of the conservative potential equation. Hampton, Va: Langley Research Center, 1986.

Dulikravich, George S. Theory of unsteady compressible irrotational flows including heat conductivity and longitudinal viscosity. New York: American Institute of Aeronautics and Astronautics, 1988.

1936-, Puu Tönu, ed. Spatial economics: Density, potential, and flow. Amsterdam: North-Holland, 1985.

Beckmann, Martin. Spatial economics: Density, potential, and flow. Amsterdam: North-Holland, 1985.

Takallu, M. A. Unsteady potential flow past a propeller blade section. Hampton, Va: Langley Research Center, 1990.

Canada. Defence Research Establishment Atlantic. Calculation of Potential Flow About Ship Hulls. S.l: s.n, 1985.

Joseph, Daniel D. Potential flows of viscous and viscoelastic fluids. Cambridge: Cambridge University Press, 2007.

Summa, J. Michael. A novel potential viscous flow coupling technique for computing helicopter flow fields. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Summa, J. Michael. A novel potential viscous flow coupling technique for computing helicopter flow fields. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Norburn, M. D. S. Mixed finite element methods for potential flow problems. Manchester: UMIST, 1996.

Hwang, H. Direct solution of unsteady transonic flow equations in frequency domain. New York: AIAA, 1989.

Chu, Li-Chuan. Integral equation solution of the full potential equation for three-dimensional, steady, transonic wing flows. Norfolk, Va: Old Dominion University, 1988.

Hu, Hong. Full-potential integral solutions for steady and unsteady transonic airfoils with and without embedded Euler domains. Norfolk, Va: Old Dominion University, 1988.

Westland, J. Clebsch variable model for unsteady inviscid transonic flow with strong shock waves. Amsterdam: National Aerospace Laboratory, 1993.

Center, Langley Research, ed. Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

United States. National Aeronautics and Space Administration., ed. On approximate factorization schemes for solving the full potential equation. Washington, DC: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. On approximate factorization schemes for solving the full potential equation. Washington, DC: National Aeronautics and Space Administration, 1997.

Kuo-Yen, Szema, and Langley Research Center, eds. Nonlinear potential analysis techniques for supersonic aerodynamic design. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

J, Strash Daniel, Yoo Sungyul, and United States. National Aeronautics and Space Administration., eds. A novel potential/viscous flow coupling technique for computing helicopter flow fields: Final report. Redmond, WA: Analytical Methods, Inc., 1993.

Ali, Thuriya A. Razzak Hasson. A flow cell to study formation potential of pulps. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1999.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, ed. General design method for three-dimensional, potential flow fields. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. General design method for three-dimensional, potential flow fields. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. General design method for three-dimensional, potential flow fields. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Dulikravich, George S. A physically consistent model for artificial dissipation in transonic potential flow computations. Cleveland, Ohio: Institute for Computational Mechanics in Propulsion, Lewis Research Center, 1988.

United States. National Aeronautics and Space Administration., ed. Potential flow downstream of the heliospheric terminal schock: A non-spherical schock / Steven Nerney and Steven T. Suess. Washington, DC: National Aeronautics and Space Administration, 1994.

Graham, D. D. Potential for leakage among principal aquifers in the Memphis area, Tennessee. Memphis, Tenn: U.S. Dept. of the Interior, Geological Survey, 1986.

Rich, Jack Samuel. Linearized velocity perturbation potential as an initial guess for a transonic iteration procedure. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, 1985.

Bewley, T. R. An application of conformal mappings to general grid generation and potential flow problems. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1990.

T, Suess Steven, and United States. National Aeronautics and Space Administration., eds. Potential flow downstream of the heliospheric terminal shock: A non-spherical shock. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Graham, D. D. Potential for leakage among principal aquifers in the Memphis area, Tennessee. Memphis, Tenn: U.S. Dept. of the Interior, Geological Survey, 1986.

D, Graham D. Potential for leakage among principal aquifers in the Memphis area, Tennessee. Memphis, Tenn: U.S. Dept. of the Interior, Geological Survey, 1986.

Schippers, H. TULIPS: a method to calculate transonic potential flow about oscillating airfoils. Amsterdam, Netherlands: National Aerospace Laboratory, 1988.

Chu, Li-Chuan. Integral equation solution of the full potential equation for transonic flows. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.

Wees, A. J. van der. A nonlinear multigrid method for three-dimensional transonic potential flow. Amsterdam: National Aerospace Laboratory, 1988.

United States. National Aeronautics and Space Administration., ed. Development of a multigrid transonic potential flow code for cascades. [Washington, DC: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. Small-amplitude disturbances in turbomachine flows with swirl. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Small-amplitude disturbances in turbomachine flows with swirl. [Washington, DC: National Aeronautics and Space Administration, 1994.

G, Keith T., Brewe D. E, and Lewis Research Center, eds. Extension of transonic flow computational concepts in the analysis of cavitated bearings. [Cleveland, Ohio: Lewis Research Center, 1990.

Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Hounjet, M. H. L. ARSPNSC: A method to calculate subsonic steady and unsteady potential flow about complex configurations. Amsterdam: National Aerospace Laboratory, 1986.

Center, Ames Research, ed. Numerical solution of the full potential equation using a chimera grid approach. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

Center, Ames Research, ed. Numerical solution of the full potential equation using a chimera grid approach. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

J, Vinson, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Regulatory Applications., University of Arizona. Dept. of Soil and Water Science., New Mexico State University. Dept. of Agronomy., and New Mexico State University. Dept. of Mechanical Engineering., eds. Flow and transport at the Las Cruces trench site: Experiment IIb. Washington, DC: Division of Regulatory Applications, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1997.

Nguyen, Yves. Potential flow around two-dimensional airfoils using a singular integral method. Austin, TX: Fluid Dynamics Group, Bureau of Engineering Research, University of Texas at Austin, 1987.

Vooren, J. Van der. Wave drag determination in the transonic full-potential flow code matrics. Amsterdam: National Aerospace Laboratory, 1990.