Books on the topic 'Low winds'
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ADMINISTRATION, FEDERAL AVIATION. Low level windshear alert system network expansion project implementation plan. Dept. of Transportation, Federal Aviation Administration, 1993.
Find full textJordan, J. R. Feasibility study for a low-altitude wind and temperature profiler. U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Wave Propagation Laboratory, 1992.
Find full textCharlton, Joe R. The performance of low-rise open span heavy steel structures in extreme winds. Available from National Technical Information Service, 1997.
Find full textWos, Kenneth A. A climatology of polar low occurrences in the Nordic Seas and an examination of katabatic winds as a triggering mechanism. Naval Postgraduate School, 1992.
Find full textGoodyer, M. J. A swept wing panel in a low speed flexible walled test section. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textGoodyer, M. J. A swept wing panel in a low speed flexible walled test section. Langley Research Center, 1987.
Find full textL, 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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textL, 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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textL, 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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textL, 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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textCenter, Langley Research, ed. Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textCenter, Langley Research, ed. Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textDoggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textDoggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textDoggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textBurel, Jorge. El viajero invisible: Breviario de los vientos. Editorial Fin de Siglo, 1996.
Find full textScott, Samuel J. Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textW, 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. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textCenter, Langley Research, ed. Flutter of a low-aspect-ratio rectangular wing. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textCenter, Langley Research, ed. Flutter of a low-aspect-ratio rectangular wing. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textCole, Stanley R. Flutter of a low-aspect-ratio rectangular wing. Langley Research Center, 1989.
Find full textBell, James H. Contraction design for small low-speed wind tunnels. Stanford University, Department of Aeronautics and Astronautics, 1988.
Find full textRoss, Holly M. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textRoss, Holly M. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textRoss, Holly M. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textRoss, Holly M. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textS, 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. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textE, McGrath Brian, and Langley Research Center, eds. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCatlin, Gregory M. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCatlin, Gregory M. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Integral method of wall interference correction in low-speed wind tunnels. National Aeronautics and Space Administration, 1987.
Find full textWatmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Aeronautical Research Laboratories, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. National Aeronautics and Space Administration, 1993.
Find full textShepherd, Kevin P. Detection of low frequency impulsive noise from large wind turbine generators. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textCenter, Ames Research, ed. Boundary-layer measurements on a transonic low-aspect ratio wing. National Aeronautics and Space Administration, Ames Research Center, 1989.
Find full textCenter, Ames Research, ed. Boundary-layer measurements on a transonic low-aspect ratio wing. National Aeronautics and Space Administration, Ames Research Center, 1989.
Find full textCenter, Ames Research, ed. Boundary-layer measurements on a transonic low-aspect ratio wing. National Aeronautics and Space Administration, Ames Research Center, 1989.
Find full textT, Steinberg J., McNutt Ralph L, and United States. National Aeronautics and Space Administration., eds. A low-mass Faraday Cup experiment for the solar wind. National Aeronautics and Space Administration, 1993.
Find full textT, Steinberg J., McNutt Ralph L, and United States. National Aeronautics and Space Administration., eds. A low-mass Faraday Cup experiment for the solar wind. National Aeronautics and Space Administration, 1993.
Find full textJ, Engebretson M., Takahashi K, and Scholer M. 1940-, eds. Solar wind sources of magnetospheric ultra-low-frequency waves. American Geophysical Union, 1994.
Find full textMidden, Raymond E. Description and calibration of the Langley hypersonic CF: A facility for simulating low. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textBell, J. H. Contraction design for small low-speed wind tunnels. National Aeronautics and Space Administration, 1988.
Find full textT, 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. National Aeronautics and Space Administration, 1992.
Find full textMidden, Raymond E. Description and calibration of the Langley hypersonic CF: A facility for simulating low ©. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full text1930-, Sandlin Doral R., and Dryden Flight Research Facility, eds. Comparison of theoretical and flight-measured local flow aerodynamics for a low-aspect-ratio fin. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Find full textCenter, Langley Research, ed. Low speed wind tunnel test of a propulsive wing/canard concept in the STOL configuration. National Aeronautics and Space Administration, Langley Research Center, 1987.
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