Books on the topic 'Hypersonic boundary-layer transition'

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

Richards, W. Lance. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Three-Dimensional Hypersonic Boundary Layer Stability and Transition. Storming Media, 1997.

A, Thompson R., and United States. National Aeronautics and Space Administration., eds. Hypersonic boundary-layer transition for X-33 phase II vehicle. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

A, Thompson R., and United States. National Aeronautics and Space Administration., eds. Hypersonic boundary-layer transition for X-33 phase II vehicle. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

A, Thompson R., and United States. National Aeronautics and Space Administration., eds. Hypersonic boundary-layer transition for X-33 phase II vehicle. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

A, Thompson R., and United States. National Aeronautics and Space Administration., eds. Hypersonic boundary-layer transition for X-33 phase II vehicle. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone: Final report. Norfolk, Va: Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University, 1996.

On the Görtler instability in hypersonic flows: Sutherland law fluids and real gas effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

On the Görtler instability in hypersonic flows: Sutherland law fluids and real gas effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, ed. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.