Libros sobre el tema "Angle of sideslip"
Crea una cita precisa en los estilos APA, MLA, Chicago, Harvard y otros
Consulte los 19 mejores mejores libros para su investigación sobre el tema "Angle of sideslip".
Junto a cada fuente en la lista de referencias hay un botón "Agregar a la bibliografía". Pulsa este botón, y generaremos automáticamente la referencia bibliográfica para la obra elegida en el estilo de cita que necesites: APA, MLA, Harvard, Vancouver, Chicago, etc.
También puede descargar el texto completo de la publicación académica en formato pdf y leer en línea su resumen siempre que esté disponible en los metadatos.
Explore libros sobre una amplia variedad de disciplinas y organice su bibliografía correctamente.
Whipple, Raymond D. Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and sideslip. Hampton, Va: Langley Research Center, 1986.
Buscar texto completoA, Whitmore Stephen y Dryden Flight Research Facility, eds. A preliminary look at techniques used to obtain airdata from flight at high angles of attack. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.
Buscar texto completoApplin, Zachary T. Wing pressure distributions from subsonic tests of a high-wing transport model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Buscar texto completoApplin, Zachary T. Wing pressure distributions from subsonic tests of a high-wing transport model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Buscar texto completoRoss, 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.
Buscar texto completoRoss, 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.
Buscar texto completoRoss, 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.
Buscar texto completoRoss, 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.
Buscar texto completoJ, Bjarke Lisa y Hugh L. Dryden Flight Research Center., eds. Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1994.
Buscar texto completoJ, Bjarke Lisa y Hugh L. Dryden Flight Research Center., eds. Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1994.
Buscar texto completoJ, Bjarke Lisa y Hugh L. Dryden Flight Research Center., eds. Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1994.
Buscar texto completoGeorge C. Marshall Space Flight Center., ed. Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.
Buscar texto completoCenter, Langley Research, ed. Computer programs for calculation of sting pitch and roll angles required to obtain angles of attack and sideslip on wind tunnel models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Buscar texto completoA, Whitmore Stephen y Jordan Frank L, eds. Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Facility, 1993.
Buscar texto completoA, Whitmore Stephen y Jordan Frank L, eds. Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Facility, 1993.
Buscar texto completoA, Whitmore Stephen y Jordan Frank L, eds. Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Facility, 1993.
Buscar texto completoA, Whitmore Stephen y Jordan Frank L, eds. Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Facility, 1993.
Buscar texto completoComputer programs for the calculation of dual sting pitch and roll angles required for an articulated sting to obtain angles of attack and sideslip on wind-tunnel models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Buscar texto completoNational Aeronautics and Space Administration (NASA) Staff. Computer Programs for the Calculation of Dual Sting Pitch and Roll Angles Required for an Articulated Sting to Obtain Angles of Attack and Sideslip on Wind-Tunnel Models. Independently Published, 2018.
Buscar texto completo