Books on the topic 'Boundary-layer transition'

Narasimha, R. Modeling the transitional boundary layer. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

O'Hare, J. E. A nonperturbing boundary-layer transition detector. Arnold Air Force Station, Tenn: Arnold Engineering Development Center, 1985.

Herbert, Th. Boundary-layer transition - analysis and prediction revisted. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

Institute for Computer Applications in Science and Engineering., ed. Modelling the transitional boundary layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

Fasel, Hermann F. Numerical simulation of nonlinear receptivity in boundary layer transition. Tucson, Ariz: University of Arizona, Engineering Experiment Station, 1990.

Holmes, Bruce J. Advanced boundary layer transition measurement methods for flight applications. New York: American Institute of Aeronautics and Astronautics, 1986.

Bertolotti, Fabio P. Simulation of boundary-layer transition: receptivity to spike stage. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1992.

United States. National Aeronautics and Space Administration., ed. The role of nonlinear critical layers in boundary layer transition. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Goldstein, Marvin E. The effect of nonlinear critical layers on boundary layer transition. [Washington, D.C: National Aeronautics and Space Administration, 1995.

J, Holmes Bruce, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Flight-measured laminar boundary-layer transition phenomena including stability theory analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

E, Krist Steven, Hussaini M. Yousuff, and Langley Research Center, eds. Resolution requirements for numerical simulations of transition. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Relationship between transition and modes of instability in supersonic boundary layers. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Program, 1993.

Evans, J. Research on boundary layer transition fixing in the DREV indraft wind tunnel. Valcartier, Quebec: Defence Research Establishment, 1988.

Adrian, R. J. Instantaneous structure of turbulent separated boundary layers: Report of research performed during the period August 3, 1995 to August 20, 1996, with support of grant number NAG 1 1530. [Washington, DC: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. Instantaneous structure of turbulent separated boundary layers: Report of research performed during the period August 3, 1995 to August 20, 1996, with support of grant number NAG 1 1530. [Washington, DC: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. Performance of renormalization group algebraic turbulence model on boundary layer transition simulation. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Center, Ames Research, ed. A brief review of some mechanisms causing boundary layer transition at high speeds. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Wendt, Volker. Experimentelle Untersuchung der Instabilitat von ebenen und konischen laminaren Hyperschallgrenzschichten. Koln, Germany: DLR, 1993.

E, O'Brien James, Reshotko Eli, and United States. National Aeronautics and Space Administration., eds. Experimental study of bypass transition in a boundary layer. [Washington, DC]: National Aeronautics and Space Administration, 1988.

E, O'Brien J., Reshotko Eli, and United States. National Aeronautics and Space Administration., eds. Some characteristics of bypass transition in a heated boundary layer. [Washington, DC]: National Aeronautics and Space Administration, 1989.

E, O'Brien J., Reshotko E, and United States. National Aeronautics and Space Administration., eds. Some characteristics of bypass transition in a heated boundary layer. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Lysenko, V. I. Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point. Washington, D.C: National Aeronautics and Space Administration, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on progress in transition modelling. Neuilly-sur-Seine, France: AGARD, 1994.

Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. and Von Karman Institute for fluid Dynamics., eds. Special course on progress in transition modelling. Neuilly sur Seine: Agard, 1994.

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

Yousuff, Hussaini M., and Langley Research Center, eds. 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. Scientific and Technical Information Program., ed. Modeling the transition region. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Program, 1993.

Zhining, Liu, and United States. National Aeronautics and Space Administration., eds. Multigrid direct numerical simulation of the whole process of flow transition in 3-D boundary layers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Marshall, Laurie A. Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Hugh L. Dryden Flight Research Center., ed. Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Hugh L. Dryden Flight Research Center., ed. Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computation of Three-Dimensional Boundary Layers Including Separation. S.l: s.n, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computation of three-dimensional boundary layers including separation. Neuilly sur Seine, France: AGARD, 1987.

Doerffer, Piotr, Pawel Flaszynski, Jean-Paul Dussauge, Holger Babinsky, Patrick Grothe, Anna Petersen, and Flavien Billard, eds. Transition Location Effect on Shock Wave Boundary Layer Interaction. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-47461-4.

D, Crouch Jeffrey, and Langley Research Center, eds. Simulation of boundary-layer transition: Receptivity to spike stage. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

D, Modarress, Trolinger Jim, and Langley Research Center, eds. Feasibility study of optical boundary layer transition detection method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Tokyo, Japan) International Workshop on "Prediction of Laminar-turbulent Transition in Boundary Layers" (2000. Prediction of laminar-turbulent transition in boundary layers. Tokyo: National Aerospace Laboratory, 2000.

Joslin, Ronald D. Active control of instabilities in laminar boundary-layer flow. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Joslin, Ronald D. Validation of three-dimensional incompressible spatial direct numerical simulation code: A comparison with linear stability and parabolic equation theories for boundary-layer transition on a flat plate. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Joslin, Ronald D. Validation of three-dimensional incompressible spatial direct numerical simulation code: A comparison with linear stability and parabolic equation theories for boundary-layer transition on a flat plate. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

L, Streett Craig, Chang Chau-Lyan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Validation of three-dimensional incompressible spatial direct numerical simulation code: A comparison with linear stability and parabolic equation theories for boundary-layer transition on a flat plate. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Joslin, Ronald D. Validation of three-dimensional incompressible spatial direct numerical simulation code: A comparison with linear stability and parabolic stability equation theories for boundary-layer transition on a flat plate. Hampton, Va: Langley Research Center, 1992.

Reed, Helen L. Final report for Navier-Stokes simulation of boundary-layer transition. Tempe, Arizona: Arizona State University, Dept. of Mechanical and Aerospace Engineering, 1990.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

El-Hady, Nabil M. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. Hampton, Va: Langley Research Center, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.