Książki na temat „Wind tunnel testing”

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.

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

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

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

Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel., red. Quality assessment for wind tunnel testing. Neuilly sur Seine: Agard, 1994.

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.

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.

American Society of Civil Engineers. Wind tunnel testing for buildings and other structures. Reston, VA: American Society of Civil Engineers, 2012.

J, Jeracki Robert, i United States. National Aeronautics and Space Administration., red. Porous wind tunnel corrections for counterrotation propeller testing. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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.

E, Cermak J., Isyumov N i American Society of Civil Engineers. Task Committee on Manual of Practice for Wind Tunnel Testing of Buildings and Structures., red. Wind tunnel studies of buildings and structures. Reston, VA: American Society of Civil Engineers, 1999.

E, Cermak J., Isyumov N i American Society of Civil Engineers. Task Committee on Manual of Practice for Wind Tunnel Testing of Buildings and Structures., red. Wind tunnel studies of buildings and structures. Reston, VA: American Society of Civil Engineers, 1998.

Jr, Rivera José A., i United States. National Aeronautics and Space Administration., red. The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel. [Washington, D.C: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., red. Design and testing of an oblique all-wing supersonic transport. San Jose, CA: MCAT Institute, 1994.

Brown, Charles E. An engineering study of hybrid adaptation of wind tunnel walls for three dimensional testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Wieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Wieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Wieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Wieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Shui zhong bing qi feng dong shi yan ji shu. Beijing Shi: Guo fang gong ye chu ban she, 2008.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Aerofoil testing in a self-streamlining flexible walled wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Center, Ames Research, red. Analysis of the free-tip rotor wind-tunnel test results. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Center, Ames Research, red. Analysis of the free-tip rotor wind-tunnel test results. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

M, Gregorek G., i United States. National Aeronautics and Space Administration., red. Wind tunnel evaluation of a truncated NACA 64-621 airfoil for wind turbine applications. [Washington, DC: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Space Shuttle Phase B Wind Tunnel Database: Summary report. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

George C. Marshall Space Flight Center., red. Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21). [Huntsville, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

E, Hyman Curtis, i Langley Research Center, red. Procedures and requirements for testing in the Langley Research Center Unitary Plan Wind Tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Mirick, Paul H. Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. Hampton, Va: Langley Research Center, 1990.

V, Vorburger T., i United States. National Bureau of Standards, red. The Wind tunnel model surface gauge for measuring roughness. [Gaithersburg, MD: U.S. Dept. of Commerce, National Bureau of Standards, 1987.

Glynn, J. L. Space shuttle phase B wind tunnel model and test information. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

H, Wentz W., i United States. National Aeronautics and Space Administration., red. Performance and aerodynamic braking of a horizontal-axis wind turbine from small-scale wind tunnel tests. [Washington, DC: National Aeronautics and Space Administration, 1987.

Schairer, Edward T. A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Institute, American Petroleum, red. Wind tunnel testing of external floating-roof storage tanks: Measurement coordination. Washington, D.C. (1220 L St., N.W., Washington 20005): American Petroleum Institute, 1993.

Fleming, Robert J. An experimental evaluation of advanced rotorcraft airfoils in the NASA Ames eleven-foot wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Center, Langley Research, red. Flutter suppression digital control law desighn and testing for the AFW wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Murthy, A. V. Effects of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing. Hampton, Va: Langley Research Center, 1986.

Migliore, Paul G. Wind tunnel aeroacoustic tests of six airfoils for use on small wind turbines: Preprint. Golden, Colo: National Renewable Energy Laboratory, 2003.

Campbell, W. A. A report on high speed wind tunnel testing of the large scale advanced prop-fan. Washington, D. C: American Institute of Aeronautics and Astronautics, 1988.

Center, Langley Research, red. Low speed wind tunnel test of a propulsive wing/canard concept in the STOL configuration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

United States. National Aeronautics and Space Administration., red. Design and fabrication of forward-swept counterrotation blade configuration for wind tunnel testing: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

A, Campbell William. Large scale advanced prop-fan (LAP) high speed wind tunnel test report. [Windsor Locks, CT]: Hamilton Standard Division, United Technologies Corporation, 1989.

Bonhaus, Daryl L. Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils. Hampton, Va: Langley Research Center, 1995.

Japan) Fūdō Kenkyū Kaigi (66th 2001 Tokyo. Dai 66-kai Fūdō Kenkyū Kaigi ronbunshū: Proceedings of the Wind Tunnel Technology Association 66th meeting. Tōkyō-to Chōfu-shi: Uchū Kōkū Kenkyū Kaihatsu Kikō, 2004.

Billman, Barbara J. Windbreak effectiveness for storage-pile fugitive-dust control: A wind tunnel study. Research Triangle Park, N.C: U.S. Environmental Protection Agency, Atmospheric Sciences Research Laboratory, 1985.

Soderman, Paul T. The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

Soderman, Paul T. The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.