Books on the topic 'Angle of sideslip'
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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.
Find full textA, Whitmore Stephen, and 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.
Find full textApplin, 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.
Find full textApplin, 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.
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 ̊. Hampton, Va: 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 ̊. Hampton, Va: 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 ̊. Hampton, Va: 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 ̊. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textJ, Bjarke Lisa, and 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.
Find full textJ, Bjarke Lisa, and 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.
Find full textJ, Bjarke Lisa, and 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.
Find full textGeorge 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.
Find full textCenter, 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.
Find full textA, Whitmore Stephen, and 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.
Find full textA, Whitmore Stephen, and 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.
Find full textA, Whitmore Stephen, and 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.
Find full textA, Whitmore Stephen, and 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.
Find full textComputer 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.
Find full textNational 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.
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