Книги з теми "Low winds"
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ADMINISTRATION, FEDERAL AVIATION. Low level windshear alert system network expansion project implementation plan. [Washington, D.C.?]: Dept. of Transportation, Federal Aviation Administration, 1993.
Charlton, Joe R. The performance of low-rise open span heavy steel structures in extreme winds. Springfield, Va: Available from National Technical Information Service, 1997.
Jordan, J. R. Feasibility study for a low-altitude wind and temperature profiler. Boulder, Colo: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Wave Propagation Laboratory, 1992.
Wos, Kenneth A. A climatology of polar low occurrences in the Nordic Seas and an examination of katabatic winds as a triggering mechanism. Monterey, Calif: Naval Postgraduate School, 1992.
Goodyer, M. J. A swept wing panel in a low speed flexible walled test section. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Goodyer, M. J. A swept wing panel in a low speed flexible walled test section. Hampton, Va: Langley Research Center, 1987.
L, Lawing Pierce, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
L, Lawing Pierce, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
L, Lawing Pierce, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
L, Lawing Pierce, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Center, Langley Research, ed. Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Center, Langley Research, ed. Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
C, Martha Ilia Nájera. Dioses y seres del viento entre los antiguos mayas. México, D.F: Universidad Nacional Autónoma de México, 2015.
Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Burel, Jorge. El viajero invisible: Breviario de los vientos. [Montevideo], Uruguay: Editorial Fin de Siglo, 1996.
Barlow, Jewel B. Low-speed wind tunnel testing. 3rd ed. New York: Wiley, 1999.
Center, Langley Research, ed. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Center, Langley Research, ed. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Cole, Stanley R. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: Langley Research Center, 1989.
Scott, Samuel J. Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
W, Nicks Oran, Imbrie P. K, and Langley Research Center, eds. Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Bell, James H. Contraction design for small low-speed wind tunnels. Stanford, Calif: Stanford University, Department of Aeronautics and Astronautics, 1988.
S, Walker Betty, Millard Betty F, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Ross, Holly M. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Ross, Holly M. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Ross, Holly M. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Ross, Holly M. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
E, McGrath Brian, and Langley Research Center, eds. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Catlin, Gregory M. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Catlin, Gregory M. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
United States. National Aeronautics and Space Administration., ed. Integral method of wall interference correction in low-speed wind tunnels. Washington, DC: National Aeronautics and Space Administration, 1987.
Watmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Melbourne, Australia: Aeronautical Research Laboratories, 1986.
United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.
United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.
United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Shepherd, Kevin P. Detection of low frequency impulsive noise from large wind turbine generators. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Center, Ames Research, ed. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Center, Ames Research, ed. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Center, Ames Research, ed. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
T, Steinberg J., McNutt Ralph L, and United States. National Aeronautics and Space Administration., eds. A low-mass Faraday Cup experiment for the solar wind. [Washington, DC: National Aeronautics and Space Administration, 1993.
T, Steinberg J., McNutt Ralph L, and United States. National Aeronautics and Space Administration., eds. A low-mass Faraday Cup experiment for the solar wind. [Washington, DC: National Aeronautics and Space Administration, 1993.
J, Engebretson M., Takahashi K, and Scholer M. 1940-, eds. Solar wind sources of magnetospheric ultra-low-frequency waves. Washington, DC, USA: American Geophysical Union, 1994.
Bell, J. H. Contraction design for small low-speed wind tunnels. [Washington, DC: National Aeronautics and Space Administration, 1988.
Midden, Raymond E. Description and calibration of the Langley hypersonic CF: A facility for simulating low. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Chereguini, Benito. Refranes de la mar al compás de los vientos. [Spain]: Noray, 1988.
Roberts, Len. Black wings. New York: Persea Books, 1989.
T, Pickett Mark, and United States. National Aeronautics and Space Administration., eds. Flow quality studies of the NASA Lewis Research Center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, 1992.
Midden, Raymond E. Description and calibration of the Langley hypersonic CF: A facility for simulating low ©. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.