Livres sur le sujet « 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.
Trouver le texte intégralCharlton, Joe R. The performance of low-rise open span heavy steel structures in extreme winds. Springfield, Va : Available from National Technical Information Service, 1997.
Trouver le texte intégralJordan, 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.
Trouver le texte intégralWos, 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.
Trouver le texte intégralGoodyer, 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.
Trouver le texte intégralGoodyer, M. J. A swept wing panel in a low speed flexible walled test section. Hampton, Va : Langley Research Center, 1987.
Trouver le texte intégralL, Lawing Pierce, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. 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.
Trouver le texte intégralL, Lawing Pierce, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. 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.
Trouver le texte intégralL, Lawing Pierce, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. 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.
Trouver le texte intégralL, Lawing Pierce, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. 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.
Trouver le texte intégralCenter, Langley Research, dir. 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.
Trouver le texte intégralCenter, Langley Research, dir. 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.
Trouver le texte intégralC, Martha Ilia Nájera. Dioses y seres del viento entre los antiguos mayas. México, D.F : Universidad Nacional Autónoma de México, 2015.
Trouver le texte intégralDoggett, 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.
Trouver le texte intégralDoggett, 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.
Trouver le texte intégralDoggett, 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.
Trouver le texte intégralBurel, Jorge. El viajero invisible : Breviario de los vientos. [Montevideo], Uruguay : Editorial Fin de Siglo, 1996.
Trouver le texte intégralBarlow, Jewel B. Low-speed wind tunnel testing. 3e éd. New York : Wiley, 1999.
Trouver le texte intégralCenter, Langley Research, dir. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1989.
Trouver le texte intégralCenter, Langley Research, dir. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1989.
Trouver le texte intégralCole, Stanley R. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va : Langley Research Center, 1989.
Trouver le texte intégralScott, 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.
Trouver le texte intégralW, Nicks Oran, Imbrie P. K et Langley Research Center, dir. 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.
Trouver le texte intégralBell, James H. Contraction design for small low-speed wind tunnels. Stanford, Calif : Stanford University, Department of Aeronautics and Astronautics, 1988.
Trouver le texte intégralS, Walker Betty, Millard Betty F et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. 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.
Trouver le texte intégralRoss, 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.
Trouver le texte intégralRoss, 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.
Trouver le texte intégralRoss, 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.
Trouver le texte intégralRoss, 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.
Trouver le texte intégralE, McGrath Brian, et Langley Research Center, dir. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1995.
Trouver le texte intégralCatlin, 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.
Trouver le texte intégralCatlin, 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.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Integral method of wall interference correction in low-speed wind tunnels. Washington, DC : National Aeronautics and Space Administration, 1987.
Trouver le texte intégralWatmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Melbourne, Australia : Aeronautical Research Laboratories, 1986.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC] : National Aeronautics and Space Administration, 1993.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC] : National Aeronautics and Space Administration, 1993.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC] : National Aeronautics and Space Administration, 1993.
Trouver le texte intégralShepherd, Kevin P. Detection of low frequency impulsive noise from large wind turbine generators. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1985.
Trouver le texte intégralCenter, Ames Research, dir. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1989.
Trouver le texte intégralCenter, Ames Research, dir. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1989.
Trouver le texte intégralCenter, Ames Research, dir. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1989.
Trouver le texte intégralT, Steinberg J., McNutt Ralph L et United States. National Aeronautics and Space Administration., dir. A low-mass Faraday Cup experiment for the solar wind. [Washington, DC : National Aeronautics and Space Administration, 1993.
Trouver le texte intégralT, Steinberg J., McNutt Ralph L et United States. National Aeronautics and Space Administration., dir. A low-mass Faraday Cup experiment for the solar wind. [Washington, DC : National Aeronautics and Space Administration, 1993.
Trouver le texte intégralJ, Engebretson M., Takahashi K et Scholer M. 1940-, dir. Solar wind sources of magnetospheric ultra-low-frequency waves. Washington, DC, USA : American Geophysical Union, 1994.
Trouver le texte intégralBell, J. H. Contraction design for small low-speed wind tunnels. [Washington, DC : National Aeronautics and Space Administration, 1988.
Trouver le texte intégralMidden, 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.
Trouver le texte intégralChereguini, Benito. Refranes de la mar al compás de los vientos. [Spain] : Noray, 1988.
Trouver le texte intégralRoberts, Len. Black wings. New York : Persea Books, 1989.
Trouver le texte intégralT, Pickett Mark, et United States. National Aeronautics and Space Administration., dir. 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.
Trouver le texte intégralMidden, 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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