Книги з теми "Angle of sideslip"

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.

A, 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.

Applin, 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.

Applin, 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.

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.

J, 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.

J, 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.

J, 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.

George 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.

Center, 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.

A, 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.

A, 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.

A, 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.

A, 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.

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. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

National 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.