Książki na temat „Turbulent Boundary Layer (TBL)”

Boundary layer analysis. Englewood Cliffs, N.J: Prentice Hall, 1993.

Boundary layer analysis. Reston, Va: American Institute of Aeronautics and Aeronautics, 2010.

Schetz, Joseph A. Boundary layer analysis. Wyd. 2. Reston, Va: American Institute of Aeronautics and Astronautics, 2011.

1945-, Harloff G. J., i Lewis Research Center, red. Hypersonic turbulent wall boundary layer computations. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1988.

1940-, Rahman M., red. Laminar and turbulent boundary layers. Southampton: Computational Mechanics Publication, 1997.

Center, Ames Research, red. The kinematics of turbulent boundary layer structure. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

Mouskos, Michael. Droplet growth in turbulent boundary layer clouds. Manchester: UMIST, 1997.

Otto, S. R. Fully nonlinear developent of the most unstable Go rtler vortex in a three dimensional boundary layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Zaman, K. B. M. O., Reshotko Eli i United States. National Aeronautics and Space Administration., red. Turbulent heat flux measurements in a transitional boundary layer. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Zaman, K. B. M. Q., Reshotko E i United States. National Aeronautics and Space Administration., red. Turbulent heat flux measurements in a transitional boundary layer. [Washington, DC]: National Aeronautics and Space Administration, 1992.

J, Dodson Lori, i United States. National Aeronautics and Space Administration., red. Hypersonic shock/boundary-layer interaction database. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

J, Dodson Lori, i Ames Research Center, red. Hypersonic shock/boundary-layer interaction database. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

J, Dodson Lori, i Ames Research Center, red. Hypersonic shock/boundary-layer interaction database. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

J, Dodson Lori, i United States. National Aeronautics and Space Administration., red. Hypersonic shock/boundary-layer interaction database. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

J, Dodson Lori, i United States. National Aeronautics and Space Administration., red. Hypersonic shock/boundary-layer interaction database. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

J, Dodson Lori, i United States. National Aeronautics and Space Administration., red. Hypersonic shock/boundary-layer interaction database. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

Boundary layers. Oxford: Boston, 1989.

Boundary layers. Washington, DC: American Institute of Aeronautics and Astronautics, 1989.

Byzova, N. L. Turbulentnost v́ pogranichnom sloe atmosfery. Leningrad: Gidrometeoizdat, 1989.

R, T͡S︡vang L., Kader B. A i Akademii͡a︡ nauk SSSR. Mezhduvedomstvennyĭ geofizicheskiĭ komitet., red. Vzaimodeĭstvie atmosfery s podstilai͡u︡shcheĭ poverkhnostʹi͡u︡: [otvetstvennye redaktory L.R. T͡S︡vang, B.A. Kader]. Moskva: Mezhduvedomstvennyĭ geofizicheskiĭ kom-t pri Prezidiume Akademii nauk SSSR, 1987.

Flohr, P. Large eddy simulation of a turbulent boundary layer. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1995.

Zhu, Shangxiang. Automatic landing through the turbulent planetary boundary layer. [Downsview, Ont.]: Institute for Aerospace Studies, 1985.

Renoud, Robert W. Boundary layer response to an unsteady turbulent environment. Monterey, Calif: Naval Postgraduate School, 1988.

Spalart, P. R. Direct simulation of a turbulent oscillating boundary layer. [Washington, DC: National Aeronautics and Space Administration, 1987.

IUTAM Symposium (1985 Palaiseau, France). Turbulent shear-layer/shock-wave interactions. Redaktorzy Délery J. 1939-, International Union of Theoretical and Applied Mechanics. i France. Office national d'études et de recherches aérospatiales. Berlin: Springer-Verlag, 1986.

Azad, Ram S. The atmospheric boundary layer for engineers. Dordrecht: Kluwer Academic Publishers, 1993.

Jarża, Alicja. Struktura i model turbulencji warstwy przyściennej z powierzchniową wymianą masy. Częstochowa: Wydawn. Politechniki Częstochowskiej, 1990.

Yousuff, Hussaini M., i Langley Research Center, red. A three-dimensional spectral algorithm for simulations of transition and turbulence. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

United States. National Aeronautics and Space Administration., red. Exploratory study of in-plane streamline curvature effects on a turbulent boundary layer at a mach number of 3: Final technical report, grant NAG-1-961 for the period January 27, 1989 - January 26, 1990. [Washington, DC: National Aeronautics and Space Administration, 1991.

Driver, David M. Experimental study of a three-dimensional shear-driven turbulent boundary layer with streamwise adverse pressure gradient. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

1922-, Kline S. J., Spalart P. R i Ames Research Center, red. A review of quasi-coherent structures in a numerically simulated turbulent boundary layer. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

United States. National Aeronautics and Space Administration., red. A three-dimensional turbulent separated flow and related measurements. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1985.

1922-, Kline S. J., Spalart P. R i Ames Research Center, red. A review of quasi-coherent structures in a numerically simulated turbulent boundary layer. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Marvin, J. G. Turbulence modeling for hypersonic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Lucio, Maestrello, i Langley Research Center, red. Responses of a finite baffled plate subject to turbulent and mean flow excitations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Eli, Reshotko, i Lewis Research Center, red. Experimental study of boundary layer transition with elevated freestream turbulence on a heated flat plate. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

McKinzie, Daniel J. Delay of turbulent boundary layer detachment by mechanical excitation: Application to rearward-facing ramp. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

United States. National Aeronautics and Space Administration., red. A three-dimensional turbulent separated flow and related measurements. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1985.

United States. National Aeronautics and Space Administration., red. Exploratory study of in-plane streamline curvature effects on a turbulent boundary layer at a mach number of 3: Final technical report, grant NAG-1-961 for the period January 27, 1989 - January 26, 1990. [Washington, DC: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., red. Exploratory study of in-plane streamline curvature effects on a turbulent boundary layer at a mach number of 3: Final technical report, grant NAG-1-961 for the period January 27, 1989 - January 26, 1990. [Washington, DC: National Aeronautics and Space Administration, 1991.

den, Berg Bernard van, red. Three-dimensional turbulent boundary layers: Calculations and experiments : analysis of an EUROVISC-Workshop. Braunschweig/Wiesbaden: F. Vieweg, 1988.

Eli, Reshotko, i Lewis Research Center, red. Experimental study of boundary layer transition with elevated freestream turbulence on a heated flat plate. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1991.

Subramaniam, C. S. Measurement of the low-wave-number structure of a turbulent boundary layer. London, U.K: Imperial College of Science and Technology, Dept. of Aeronautics, 1985.

Wu, Sean F. Responses of finite baffled plate subject to turbulent and mean flow excitations. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1993.

Kudashev, E. B. Turbulentnye pristenochnye pulʹsat︠s︡ii davlenii︠a︡: V aspekte zadach kontroli︠a︡ aėrogidrodinamicheskikh shumov. Moskva: Nauch. mir, 2007.

1922-, Kline S. J., Spalart P. R i Ames Research Center, red. A review of quasi-coherent structures in a numerically simulated turbulent boundary layer. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

1940-, Shih Tsan-Hsing, i United States. National Aeronautics and Space Administration., red. A new time scale based [kappa-epsilon] model for near wall turbulence. [Washington, DC: National Aeronautics and Space Administration, 1992.

Yousuff, Hussaini M., i Langley Research Center, red. A three-dimensional spectral algorithm for simulations of transition and turbulence. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Hall, Philip. On the instability of boundary layers on heated flat plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Center, Ames Research, red. Investigation of low-speed turbulent separated flow around airfoils. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.