Książki na temat „Wind tunnel”

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

Ajay, Kumar, Kegelman Jerome T i United States. National Aeronautics and Space Administration., red. 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 i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, red. 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 i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. 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, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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 i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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 i United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., red. 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 i Langley Research Center, red. 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 i Langley Research Center, red. 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 i Langley Research Center, red. 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., red. 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., red. 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., red. 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, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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, i United States. National Aeronautics and Space Administration., red. 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. Wyd. 3. New York: Wiley, 1999.

Lewis Research Center. Aeropropulsion Facilities & Experiments Division, red. 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, i United States. National Aeronautics and Space Administration., red. Automation of some operations of a wind tunnel using artificial neural networks. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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

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

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

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

R, McClinton Charles, i United States. National Aeronautics and Space Administration., red. 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, i Hermann von Helmholtz-Gemeinschaft Deutscher Forschungszentren., red. 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, i Hermann von Helmholtz-Gemeinschaft Deutscher Forschungszentren., red. 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, i Ames Research Center, red. 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., i Langley Research Center, red. Microcomputer based controller for the Langley 0.3-meter Transonic Cryogenic Tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.