Books on the topic 'Computational fluid dynamics; Wave loading'

Paxson, Daniel E. Wave augmented diffusers for centrifugal compressors. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Paxson, Daniel E. A numerical model for dynamic wave rotor analysis. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Paxson, Daniel E. A numerical model for dynamic wave rotor analysis. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Wilson, Jack. Optimization of wave rotors for use as gas turbine engine topping cycles. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Scott, James R. Compressible flows with periodic vortical disturbances around lifting airfoils. [Cleveland, Ohio: Lewis Research Center, 1991.

Harloff, G. J. Numerical simulation of supersonic flow using a new analytical bleed boundary condition. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Kussoy, Marvin. Hypersonic flows as related to the national aerospace plane: Semi-annual research report for the period August 1, 1990 - February 28, 1991. Sunnyvale, Calif: Eloret Institute, 1991.

Holland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Computational Wave Dynamics. World Scientific Publishing Co Pte Ltd, 2013.

executive, Health and safety. Some Calculations of Fluid Loading Using Computational Fluid Dynamics. Health and Safety Executive (HSE), 1996.

High Accuracy Computing Methods: Fluid Flows and Wave Phenomena. University of Cambridge ESOL Examinations, 2013.

Numerical assessment of four-part through-flow wave rotor cycles with passage height variation. [Washington, DC]: National Aeronautics and Space Administration, 1997.

Numerical simulation of low-density shock-wave interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Numerical simulation of low-density shock-wave interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Smadar, Karni, and Institute for Computer Applications in Science and Engineering., eds. On the dynamics of a shock-bubble interaction. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

L, Roberts, and Joint Institute for Aeronautics and Acoustics., eds. A CFD study of tilt rotor flowfields. Stanford, CA: Stanford University, Dept. of Aeronautics and Astronautics, 1989.

Krishnan, Radhakrishnan, and NASA Glenn Research Center, eds. Computational study of near-limit propagation of detonation in hydrogen-air mixtures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1995.

A note on the wave action density of a viscous instability mode on a laminar free-shear flow. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. A note on the wave action density of a viscous instability mode on a laminar free-shear flow. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Shock wave interaction with an abrupt area change. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

United States. National Aeronautics and Space Administration., ed. Computational modeling and validation for hypersonic inlets. [Washington, D.C: National Aeronautics and Space Administration, 1990.

Simulation of glancing shock wave and boundary layer interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

United States. National Aeronautics and Space Administration., ed. Development of a grid-independent approximate Riemann solver. [Washington, DC: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Development of a grid-independent approximate Riemann solver. [Washington, DC: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Numerical study of stratified charge combustion in wave rotors. [Washington, DC]: National Aeronautics and Space Administration, 1997.

Numerical calculations of shock-wave/boundary-layer flow interactions. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

Institute for Computer Applications in Science and Engineering., ed. A Cartesian grid approach with hierarchical refinement for compressible flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Second Computational Aeroacoustics (CAA) Workshop on Benchmark Problems: Proceedings of a workshop ... held in Tallahassee, Florida, November 4-5, 1996. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

M, Bahm Catherine, Heinle Robert A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Determination of stores pointing error due to wing flexibility under flight load. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

Yousuff, Hussaini M., and Institute for Computer Applications in Science and Engineering., eds. Non-linear evolution of a second mode wave in supersonic boundary layers. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1989.

Yousuff, Hussaini M., and Institute for Computer Applications in Science and Engineering., eds. Non-linear evolution of a second mode wave in supersonic boundary layers. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1989.

Center, Langley Research, ed. Mach 10 computational study of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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

Richard, Hawkins, and Langley Research Center, eds. Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Richard, Hawkins, and Langley Research Center, eds. Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Relativistic Dynamics of a Charged Sphere: Updating the Lorentz-Abraham Model (Lecture Notes in Physics). Springer, 2005.

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code. [Washington, DC]: National Aeronautics and Space Administration, 1994.

H, Anderson Bernhard, Shaw Robert J. 1946-, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Hypersonic flows as related to the national aerospace plane. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of shock/turbulent boundary layer interaction: Final year report for NASA grant NAG-1-1472. Boulder, Colo: Dept. of Aerospace Engineering Sciences, University of Colorado, 1993.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of shock/turbulent boundary layer interaction: Final year report for NASA grant NAG-1-1472. Boulder, Colo: Dept. of Aerospace Engineering Sciences, University of Colorado, 1993.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of shock/turbulent boundary layer interaction: Final year report for NASA grant NAG-1-1472. Boulder, Colo: Dept. of Aerospace Engineering Sciences, University of Colorado, 1993.

Center, Langley Research, ed. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.