Libros sobre el tema "Low winds"

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 y 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 y 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 y 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 y 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. 3^a 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 y 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 y 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 y 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 y 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 y 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 y 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 y 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.