Bücher zum Thema „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.
Den vollen Inhalt der Quelle findenCharlton, Joe R. The performance of low-rise open span heavy steel structures in extreme winds. Springfield, Va: Available from National Technical Information Service, 1997.
Den vollen Inhalt der Quelle findenJordan, 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.
Den vollen Inhalt der Quelle findenWos, 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.
Den vollen Inhalt der Quelle findenGoodyer, 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.
Den vollen Inhalt der Quelle findenGoodyer, M. J. A swept wing panel in a low speed flexible walled test section. Hampton, Va: Langley Research Center, 1987.
Den vollen Inhalt der Quelle findenL, Lawing Pierce, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenL, Lawing Pierce, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenL, Lawing Pierce, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenL, Lawing Pierce, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. 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.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. 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.
Den vollen Inhalt der Quelle findenC, Martha Ilia Nájera. Dioses y seres del viento entre los antiguos mayas. México, D.F: Universidad Nacional Autónoma de México, 2015.
Den vollen Inhalt der Quelle findenDoggett, 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.
Den vollen Inhalt der Quelle findenDoggett, 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.
Den vollen Inhalt der Quelle findenDoggett, 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.
Den vollen Inhalt der Quelle findenBurel, Jorge. El viajero invisible: Breviario de los vientos. [Montevideo], Uruguay: Editorial Fin de Siglo, 1996.
Den vollen Inhalt der Quelle findenBarlow, Jewel B. Low-speed wind tunnel testing. 3. Aufl. New York: Wiley, 1999.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Den vollen Inhalt der Quelle findenCole, Stanley R. Flutter of a low-aspect-ratio rectangular wing. Hampton, Va: Langley Research Center, 1989.
Den vollen Inhalt der Quelle findenScott, 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.
Den vollen Inhalt der Quelle findenW, Nicks Oran, Imbrie P. K und Langley Research Center, Hrsg. 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.
Den vollen Inhalt der Quelle findenBell, James H. Contraction design for small low-speed wind tunnels. Stanford, Calif: Stanford University, Department of Aeronautics and Astronautics, 1988.
Den vollen Inhalt der Quelle findenS, Walker Betty, Millard Betty F und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. 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.
Den vollen Inhalt der Quelle findenRoss, 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.
Den vollen Inhalt der Quelle findenRoss, 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.
Den vollen Inhalt der Quelle findenRoss, 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.
Den vollen Inhalt der Quelle findenRoss, 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.
Den vollen Inhalt der Quelle findenE, McGrath Brian, und Langley Research Center, Hrsg. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Den vollen Inhalt der Quelle findenCatlin, 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.
Den vollen Inhalt der Quelle findenCatlin, 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.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Integral method of wall interference correction in low-speed wind tunnels. Washington, DC: National Aeronautics and Space Administration, 1987.
Den vollen Inhalt der Quelle findenWatmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Melbourne, Australia: Aeronautical Research Laboratories, 1986.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenShepherd, Kevin P. Detection of low frequency impulsive noise from large wind turbine generators. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Boundary-layer measurements on a transonic low-aspect ratio wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Den vollen Inhalt der Quelle findenT, Steinberg J., McNutt Ralph L und United States. National Aeronautics and Space Administration., Hrsg. A low-mass Faraday Cup experiment for the solar wind. [Washington, DC: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenT, Steinberg J., McNutt Ralph L und United States. National Aeronautics and Space Administration., Hrsg. A low-mass Faraday Cup experiment for the solar wind. [Washington, DC: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenJ, Engebretson M., Takahashi K und Scholer M. 1940-, Hrsg. Solar wind sources of magnetospheric ultra-low-frequency waves. Washington, DC, USA: American Geophysical Union, 1994.
Den vollen Inhalt der Quelle findenBell, J. H. Contraction design for small low-speed wind tunnels. [Washington, DC: National Aeronautics and Space Administration, 1988.
Den vollen Inhalt der Quelle findenMidden, 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.
Den vollen Inhalt der Quelle findenChereguini, Benito. Refranes de la mar al compás de los vientos. [Spain]: Noray, 1988.
Den vollen Inhalt der Quelle findenRoberts, Len. Black wings. New York: Persea Books, 1989.
Den vollen Inhalt der Quelle findenT, Pickett Mark, und United States. National Aeronautics and Space Administration., Hrsg. 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.
Den vollen Inhalt der Quelle findenMidden, 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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