Books on the topic 'Wind tunnel'

Ajay, Kumar, Kegelman Jerome T, and United States. National Aeronautics and Space Administration., eds. The Langley wind tunnel enterprise. [Washington, DC: National Aeronautics and Space Administration, 1998.

Ajay, Kumar, Kegelman Jerome T, and United States. National Aeronautics and Space Administration., eds. The Langley wind tunnel enterprise. [Washington, DC: National Aeronautics and Space Administration, 1998.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. Neuilly-sur-Seine, France: AGARD, 1994.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. Neuilly-sur-Seine: AGARD, 1994.

Hufnagel, Klaus. Wind Tunnel Balances. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-97766-5.

Everhart, Joel L. Slotted-wall flow-field measurements in a transonic wind tunnel. Hampton, Va: Langley Research Center, 1991.

B, Igoe William, Flechner Stuart G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Slotted-wall flow-field measurements in a transonic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

B, Igoe William, Flechner Stuart G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Slotted-wall flow-field measurements in a transonic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

E, Mineck Raymond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Adaptive wind tunnel walls: A selected, annotated bibliograpy. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

A, Kilgore Robert, Moore Deborah L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Cryogenic wind tunnels: A comprehensive, annotated bibliography. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

A, Kilgore Robert, Cole Karen L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Cryogenic wind tunnels: A selected, annotated bibliography. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Brooks, Cuyler W. The NASA Langley 8-foot transonic pressure tunnel calibration. Hampton: National Aeronautics and Space Administration, Langley Research Center, 1994.

1952-, Harris Charles D., Reagon Patricia G, and Langley Research Center, eds. The NASA Langley 8-foot transonic pressure tunnel calibration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

1952-, Harris Charles D., Reagon Patricia G, and Langley Research Center, eds. The NASA Langley 8-foot transonic pressure tunnel calibration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

1952-, Harris Charles D., Reagon Patricia G, and Langley Research Center, eds. The NASA Langley 8-foot transonic pressure tunnel calibration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Brooks, Cuyler W. The NASA Langley 8-Foot Transonic Pressure Tunnel calibration. Hampton, Va: Langley Research Center, 1994.

Galway, R. D. The IAR High Reynolds Number Two-Dimensional Test Facility - a description of equipment and procedures common to most 2-D airfoil tests. Ottawa, Ont: National Research Council Canada, Institute for Aerospace Research, 1990.

Capone, Francis J. The NASA Langley 16-Foot Transonic Tunnel: Historical overview, facility description, calibration, flow characteristics, and test capabilities. Hampton, Va: Langley Research Center, 1995.

Watmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Melbourne, Australia: Aeronautical Research Laboratories, 1986.

Galway, R. D. The IAR high Reynolds number two-dimensional test facility - a description of equipment and procedures common to most 2-D airfoil tests. Ottawa: National Research Council of Canada, Institute for Aerospace Research, 1990.

Al-Saadi, Jassim A. Wall interference and boundary simulation in a transonic wind tunnel with a discretely slotted test section. Hampton, Va: Langley Research Center, 1993.

Norris, R. B. The flying wind tunnel. New York: AIAA, 1989.

Jacobi, L. Y. I.A.I. hypersonic wind tunnel. Ben Gurion Airport, Israel: Israel Aircraft Industries Ltd, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Britcher, Colin P. Applications of magnetic suspension technology to large scale facilities: Progress, problems and promises. [Washington, DC: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Britcher, Colin P. Application of magnetic suspension and balance systems to ultra-high Reynolds number facilities. [Washington, D.C: National Aeronautics and Space Administration, 1996.

American Institute of Aeronautics and Astronautics., ed. Recommended practice: Wind tunnel testing. Reston, VA: American Institute of Aeronautics and Astronautics, 2003.

Tuttle, Marie H. Adaptive wall wind tunnels: A selected annotated bibliography. Hampton, Va: Langley Research Center, 1986.

Green, Lawrence L. Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels. Hampton, Va: Langley Research Center, 1991.

Kuczka, Detlef. Hybridverfahren fur instationare Messungen in trassonischen Windkanalen am Beispiel der harmonischen Nickschwingung. Koln: DFVLR, 1988.

Bell, James H. Contraction design for small low-speed wind tunnels. Stanford, Calif: Stanford University, Department of Aeronautics and Astronautics, 1988.

S, Hill Acquilla, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Center, Lewis Research, and United States. National Aeronautics and Space Administration., eds. Flow field surveys of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1993 test). [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Newton, James E. Study of ice accretion on icing wind tunnel components. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Barlow, Jewel B. Low-speed wind tunnel testing. 3rd ed. New York: Wiley, 1999.

Lewis Research Center. Aeropropulsion Facilities & Experiments Division, ed. The 1x1 supersonic wind tunnel. Cleveland, Ohio (21000 Brookpark Rd., Cleveland 44135): Lewis Research Center, Aeropropulsion Facilities & Experiments Division, 1993.

Baumeister, Kenneth J. Reverberation effects on directionality and response of stationary monopole and dipole sources in a wind tunnel. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

E, Buggele Alvin, and United States. National Aeronautics and Space Administration., eds. Automation of some operations of a wind tunnel using artificial neural networks. [Washington, D.C: National Aeronautics and Space Administration, 1996.

E, Buggele Alvin, and United States. National Aeronautics and Space Administration., eds. Automation of some operations of a wind tunnel using artificial neural networks. [Washington, D.C: National Aeronautics and Space Administration, 1996.

R, McClinton Charles, and United States. National Aeronautics and Space Administration., eds. Hyper-X wind tunnel program. Washington, DC: American Institute of Aeronautics and Astronautics, 1998.

United States. National Aeronautics and Space Administration., ed. Wind tunnel testing and research. [Washington, DC: National Aeronautics and Space Administration, 1994.

R, McClinton Charles, and United States. National Aeronautics and Space Administration., eds. Hyper-X wind tunnel program. Washington, DC: American Institute of Aeronautics and Astronautics, 1998.

R, McClinton Charles, and United States. National Aeronautics and Space Administration., eds. Hyper-X wind tunnel program. Washington, DC: American Institute of Aeronautics and Astronautics, 1998.

MacKinnon, A. Wind tunnel tests on a variable camber wing. Cranfield, Bedford, England: College of Aeronautics, Cranfield University, 1993.

Ali, Gülhan, and Hermann von Helmholtz-Gemeinschaft Deutscher Forschungszentren., eds. RESPACE, key technologies for reusable space systems: Results of a virtual institute programme of the German Helmholtz-Association, 2003-2007. Berlin: Springer, 2008.

Ali, Gülhan, and Hermann von Helmholtz-Gemeinschaft Deutscher Forschungszentren., eds. RESPACE, key technologies for reusable space systems: Results of a virtual institute programme of the German Helmholtz-Association, 2003-2007. Berlin: Springer, 2008.

A, Laub James, and Ames Research Center, eds. NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

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.

Allen, Kilgore W., and Langley Research Center, eds. Microcomputer based controller for the Langley 0.3-meter Transonic Cryogenic Tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.