Livros sobre o tema "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.
Encontre o texto completo da fonteCharlton, Joe R. The performance of low-rise open span heavy steel structures in extreme winds. Springfield, Va: Available from National Technical Information Service, 1997.
Encontre o texto completo da fonteJordan, 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.
Encontre o texto completo da fonteWos, 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.
Encontre o texto completo da fonteGoodyer, 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.
Encontre o texto completo da fonteGoodyer, M. J. A swept wing panel in a low speed flexible walled test section. Hampton, Va: Langley Research Center, 1987.
Encontre o texto completo da fonteL, Lawing Pierce, e 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.
Encontre o texto completo da fonteL, Lawing Pierce, e 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.
Encontre o texto completo da fonteL, Lawing Pierce, e 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.
Encontre o texto completo da fonteL, Lawing Pierce, e 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.
Encontre o texto completo da fonteCenter, 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.
Encontre o texto completo da fonteCenter, 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.
Encontre o texto completo da fonteC, Martha Ilia Nájera. Dioses y seres del viento entre los antiguos mayas. México, D.F: Universidad Nacional Autónoma de México, 2015.
Encontre o texto completo da fonteDoggett, 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.
Encontre o texto completo da fonteDoggett, 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.
Encontre o texto completo da fonteDoggett, 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.
Encontre o texto completo da fonteBurel, Jorge. El viajero invisible: Breviario de los vientos. [Montevideo], Uruguay: Editorial Fin de Siglo, 1996.
Encontre o texto completo da fonteBarlow, Jewel B. Low-speed wind tunnel testing. 3a ed. New York: Wiley, 1999.
Encontre o texto completo da fonteCenter, Langley Research, ed. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Encontre o texto completo da fonteCenter, Langley Research, ed. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Encontre o texto completo da fonteCole, Stanley R. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: Langley Research Center, 1989.
Encontre o texto completo da fonteScott, 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.
Encontre o texto completo da fonteW, Nicks Oran, Imbrie P. K e 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.
Encontre o texto completo da fonteBell, James H. Contraction design for small low-speed wind tunnels. Stanford, Calif: Stanford University, Department of Aeronautics and Astronautics, 1988.
Encontre o texto completo da fonteS, Walker Betty, Millard Betty F e 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.
Encontre o texto completo da fonteRoss, 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.
Encontre o texto completo da fonteRoss, 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.
Encontre o texto completo da fonteRoss, 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.
Encontre o texto completo da fonteRoss, 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.
Encontre o texto completo da fonteE, McGrath Brian, e 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.
Encontre o texto completo da fonteCatlin, 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.
Encontre o texto completo da fonteCatlin, 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.
Encontre o texto completo da fonteUnited 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.
Encontre o texto completo da fonteWatmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Melbourne, Australia: Aeronautical Research Laboratories, 1986.
Encontre o texto completo da fonteUnited 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.
Encontre o texto completo da fonteUnited 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.
Encontre o texto completo da fonteUnited 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.
Encontre o texto completo da fonteShepherd, Kevin P. Detection of low frequency impulsive noise from large wind turbine generators. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Encontre o texto completo da fonteCenter, 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.
Encontre o texto completo da fonteCenter, 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.
Encontre o texto completo da fonteCenter, 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.
Encontre o texto completo da fonteT, Steinberg J., McNutt Ralph L e 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.
Encontre o texto completo da fonteT, Steinberg J., McNutt Ralph L e 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.
Encontre o texto completo da fonteJ, Engebretson M., Takahashi K e Scholer M. 1940-, eds. Solar wind sources of magnetospheric ultra-low-frequency waves. Washington, DC, USA: American Geophysical Union, 1994.
Encontre o texto completo da fonteBell, J. H. Contraction design for small low-speed wind tunnels. [Washington, DC: National Aeronautics and Space Administration, 1988.
Encontre o texto completo da fonteMidden, 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.
Encontre o texto completo da fonteChereguini, Benito. Refranes de la mar al compás de los vientos. [Spain]: Noray, 1988.
Encontre o texto completo da fonteRoberts, Len. Black wings. New York: Persea Books, 1989.
Encontre o texto completo da fonteT, Pickett Mark, e 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.
Encontre o texto completo da fonteMidden, 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.
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