Books on the topic 'Quiet Tunnels'

Wolf, Stephen W. D. Supersonic wind tunnel nozzles: A selected, annotated bibliography to aid in the development of quiet wind tunnel technology. Washington, D.C: National Aeronautics and Space Administration, 1990.

Schneider, Steven P. A quiet flow Ludwieg tube for study of transition in compressible boundary layers: Design and feasibility. West Lafayette, IN: School of Aeronautics and Astronautics, Purdue University, 1991.

Schneider, Steven P. Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

Schneider, Steven P. Supersonic quiet-tunnel development for laminar-turbulent transition research: Final report for NASA Langley grant NAG-1-1607. [Washington, DC: National Aeronautics and Space Administration, 1995.

Barna, P. S. Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Progress report on the D.S.M.A. design. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

United States. National Aeronautics and Space Administration., ed. A quiet flow Ludwieg tube for study of transition in compressible boundary layers: Design and feasibility. [Washington, D.C: National Aeronautics and Space Administration, 1990.

National Aeronautics and Space Administration (NASA) Staff. Development of Quiet-Flow Supersonic Wind Tunnels for Laminar-Turbulent Transition Research. Independently Published, 2018.

Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Supersonic quiet-tunnel development for laminar-turbulent transition research: Final report for NASA Langley grant NAG-1-1607. [Washington, DC: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. Supersonic quiet-tunnel development for laminar-turbulent transition research: Final report for NASA Langley grant NAG-1-1607. [Washington, DC: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. San Jose, CA: MCAT Institute, 1992.

United States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. San Jose, CA: MCAT Institute, 1993.

United States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. San Jose, CA: MCAT Institute, 1991.

United States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle: Final report. San Jose, CA: MCAT Institute, 1995.

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Report on the modified D.S.M.A. design. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Report on the modified D.S.M.A. design. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Center, Langley Research, ed. Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Progress report on the D.S.M.A. design. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Computational Evaluation of Quiet Tunnel Hypersonic Boundary Layer Stability Experiments. Storming Media, 2000.

National Aeronautics and Space Administration (NASA) Staff. Quiet Tunnel Investigation of Hypersonic Boundary-Layer Stability over a Cooled, Flared Cone. Independently Published, 2018.

A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel. Reston, VA: American Institute of Astronautics and Aeronautics, 1997.

A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel. Reston, VA: American Institute of Astronautics and Aeronautics, 1997.

A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel. Reston, VA: American Institute of Astronautics and Aeronautics, 1997.

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.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

National Aeronautics and Space Administration (NASA) Staff. Hypersonic Boundary-Layer Stability Experiments on a Flared-Cone Model at Angle of Attack in a Quiet Wind Tunnel. Independently Published, 2018.

Oattes, Gavin. Life Will See You Now: Quit Waiting for the Light at the End of the Tunnel and Light That F*cker up for Yourself. Wiley & Sons, Incorporated, John, 2020.

Oattes, Gavin. Life Will See You Now: Quit Waiting for the Light at the End of the Tunnel and Light That F*cker up for Yourself. Wiley & Sons, Incorporated, John, 2020.

Oattes, Gavin. Life Will See You Now: Quit Waiting for the Light at the End of the Tunnel and Go Light the Fucker up for Yourself. Wiley & Sons, Limited, John, 2020.