Books on the topic 'High-speed flow'

Chapman, C. J. High speed flow. Cambridge: Cambridge University Press, 2000.

1949-, Bonnet Jean-Paul, and ScienceDirect (Online service), eds. Compressibility, turbulence and high speed flow. Amsterdam: Elsevier, 2009.

S, Rosen Bruce, ed. F-14A aircraft high-speed flow simulations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Chaussee, D. S. High speed viscous flow calculations about complex configurations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

Cherrett, M. A. Unsteady viscous flow in a high speed core compressor. Farnborough, Hampshire: Procurement Executive, Ministry of Defence, 1990.

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

United States. National Aeronautics and Space Administration., ed. Embedded function methods for compressible high speed turbulent flow. [Washington, DC?: National Aeronautics and Space Administration, 1990.

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

Pergament, Harold S. Hybrid two-equation turbulence model for high speed propulsive jets. New York: AIAA, 1986.

Hamed, A. High speed nozzles task: Final report. [Cincinnati, Ohio?]: University of Cincinnati, 1995.

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

Simin, Mokhtari, and Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. ULTRA-SHARP nonoscillatory convection schemes for high-speed steady multidimensional flow. [Washington, D.C.]: NASA, 1990.

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

Simin, Mokhtari, and Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. ULTRA-SHARP nonoscillatory convection schemes for high-speed steady multidimensional flow. [Washington, D.C.]: NASA, 1990.

Leonard, B. P. ULTRA-SHARP nonoscillatory convection schemes for high-speed steady multidimensional flow. [Washington, D.C.]: NASA, 1990.

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.

Brian, Ray. Guidelines for selection of speed reduction treatments at high-speed intersections. Washington, D.C: Transportation Research Board, 2008.

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

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.

Dash, Sanford M. Observations on practical turbulence modeling for high-speed jet/plume flowfields. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

R, Edwards Jack, and NASA Glenn Research Center, eds. Numerical speed of sound and its application to schemes for all speeds. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

R, Edwards Jack, and NASA Glenn Research Center, eds. Numerical speed of sound and its application to schemes for all speeds. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

A, Delaney Robert, and United States. National Aeronautics and Space Administration., eds. Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. [Washington, DC: National Aeronautics and Space Administration, 1993.

Center, NASA Glenn Research, ed. First NASA/Industry High Speed Research Program Nozzle Symposium. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Center, NASA Glenn Research, ed. First NASA/Industry High Speed Research Program Nozzle Symposium. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Center, Lewis Research, ed. PSP measurement of stator vane surface pressures in a high speed fan. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Rosa, M. D. Di. CW laser strategies for simultaneous multi-parameter measurements in high-speed gas flows. Washington: AIAA, 1992.

United States. National Aeronautics and Space Administration., ed. Single-shot spectrally resolved UV Rayleigh scattering measurements in high speed flow. [Washington, D.C: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Single-shot spectrally resolved UV Rayleigh scattering measurements in high speed flow. [Washington, D.C: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Single-shot spectrally resolved UV Rayleigh scattering measurements in high speed flow. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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

Yungster, Shaye. Numerical simulation of shock-induced combustion generated by high-speed projectiles in detonable gas mixtures. New York: AIAA, 1989.

A, Delaney Robert, Bettner James L, and Lewis Research Center, eds. Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems.: Final report. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

A, Delaney Robert, and United States. National Aeronautics and Space Administration., eds. Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems.: Final report. [Washington, DC: National Aeronautics and Space Administration, 1993.

D, Wolter John, and Lewis Research Center, eds. Design and checkout of a high speed research nozzle evaluation rig. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.

Center, Langley Research, ed. Unstructured grid viscous flow simulation over high-speed research technology concept airplane at high-lift conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Moitra, Anutosh. Application of a Runge-Kutta scheme for high-speed inviscid internal flows. Hampton, Va: ICASE, 1986.

N, Tiwari, and United States. National Aeronautics and Space Administration., eds. Investigation of high-speed free shear flows using improved pressure-strain correlated Reynolds stress turbulence models. Norfolk, Va: Old Dominion University Research Foundation, 1993.

N, Tiwari, and United States. National Aeronautics and Space Administration., eds. Investigation of high-speed free shear flows using improved pressure-strain correlated Reynolds stress turbulence models. Norfolk, Va: Old Dominion University Research Foundation, 1993.

N, Tiwari S., and United States. National Aeronautics and Space Administration., eds. Investigation of high-speed free shear flows using improved pressure-strain correlated Reynolds stress turbulence models. Norfolk, Va: Old Dominion University Research Foundation, 1993.

J, Panda, Elam Kristie A, and NASA Glenn Research Center, eds. Rayleigh scattering diagnostic for dynamic measurement of velocity fluctuations in high speed jets. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. 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.

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

F, Hatay Ferhat, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of stability and stabiity control of high speed compressible rotating couette flow: Final report for NASA grant NAG-1-1103. [Washington, DC: National Aeronautics and Space Administration, 1993.

A, Yoder Dennis, and United States. National Aeronautics and Space Administration., eds. Use of Navier-Stokes methods for the calculation of high-speed nozzle flow fields. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

A, Yoder Dennis, and United States. National Aeronautics and Space Administration., eds. Use of Navier-Stokes methods for the calculation of high-speed nozzle flow fields. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

A, Yoder Dennis, and United States. National Aeronautics and Space Administration., eds. Use of Navier-Stokes methods for the calculation of high-speed nozzle flow fields. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

E, Lamar John, and Langley Research Center, eds. Flow-visualization techniques used at high speed by configuration aerodynamics wind-tunnel-test team. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

Heyes, Andrew Lawrence. Las er anenometry in the high speed vortical flow around a lifting delta wing. Manchester: University of Manchester, 1994.

E, Lamar John, and Langley Research Center, eds. Flow-visualization techniques used at high speed by configuration aerodynamics wind-tunnel-test team. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.