Bücher zum Thema „Wing test“

Center, 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.

L, 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.

L, 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.

L, 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.

L, 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.

W, Kehoe M., and Langley Research Center, eds. Flight test of a decoupler pylon for wing/store flutter suppression. National Aeronautics and Space Administration, Langley Research Center, 1986.

E, Erickson R., and Ames Research Center, eds. NASA rotor systems research aircraft fixed-wing configuration flight-test results. National Aeronautics and Space Administration, Ames Research Center, 1987.

Lance, Michael B. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Y, Sung Daniel, Stroub Robert H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Y, Sung Daniel, Stroub Robert H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Lance, Michael B. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. Langley Research Center, 1991.

Y, Sung Daniel, Stroub Robert H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

B, Smeltzer D., Smith Ronald C, and Ames Research Center, eds. Test results at transonic speeds on a contoured over-the-wing propfan model. National Aeronautics and Space Administration, Ames Research Center, 1988.

G, Kvaternik Raymond, and Langley Research Center, eds. A historical overview of Aeroelasticity Branch and Transonic Dynamics Tunnel contributions to rotorcraft technology and development. National Aeronautics and Space Administration, Langley Research Center, 2001.

E, Walker Charlotte, and Langley Research Center, eds. Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations. National Aeronautics and Space Administration, Langley Research Center, 1999.

J, Bondi M., and Ames Research Center, eds. TRENDS: The aeronautical post-test database management system. National Aeronautics and Space Administration, Ames Research Center, 1990.

J, Bondi M., and Ames Research Center, eds. TRENDS: The aeronautical post-test database management system. National Aeronautics and Space Administration, Ames Research Center, 1990.

Yip, Long P. Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform. Langley Research Center, 1990.

Yip, Long P. Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform. Langley Research Center, 1990.

P, Yip Long, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

P, Yip Long, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

P, Yip Long, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

G, Bush Harold, and Langley Research Center, eds. Structural test documentation and results for the McDonnell Douglas all-composite wing stub box. National Aeronautics and Space Administration, Langley Research Center, 1997.

Larson, Richard R. Flight control system development and flight test experience with the F-111 mission adaptive wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

F, Felker Fort, and Ames Research Center, eds. Performance and loads data from a hover test of a 0.658-scale V-22 rotor and wing. National Aeronautics and Space Administration, Ames Research Center, 1987.

F-8, Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards Calif ). Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration: Proceedings of an anniversary celebration held at NASA Dryden Flight Research Center, Edwards, California, May 27, 1992. The Division, 1996.

F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards, Calif.). Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration: Proceedings of an anniversary celebration held at NASA Dryden Flight Research Center, Edwards, California, May 27, 1992. The Division, 1996.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, ed. Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration: Proceedings of an anniversary celebration held at NASA Dryden Flight Research Center, Edwards, California, May 27, 1992. The Division, 1996.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration: Proceedings of an anniversary celebration held at NASA Dryden Flight Research Center, Edwards, California, May 27, 1992. The Division, 1996.

F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards, Calif.). Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration: Proceedings of an anniversary celebration held at NASA Dryden Flight Research Center, Edwards, California, May 27, 1992. The Division, 1996.

F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards, Calif.). Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration: Proceedings of an anniversary celebration held at NASA Dryden Flight Research Center, Edwards, California, May 27, 1992. The Division, 1996.

Bolonkin, Alexander. Estimated benefits of variable-geometry wing camber control for transport aircraft. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

MacKinnon, A. Wind tunnel tests on a variable camber wing. College of Aeronautics, Cranfield University, 1993.

Peter, Bradshaw. Flow over swept flaps and flap tips: Final technical report to NASA Langley Research Center on NAG-1-1614. National Aeronautics and Space Administration, Langley Research Center, 1995.

Mineck, Raymond E. Wind-tunnel investigation of aerodynamic efficiency of three planar elliptical wings with curvature of quarter-chord line. Langley Research Center, 1993.

Buttrill, Carey S. Aeroservoelastic simulation of an active flexible wing wind tunnel model. Langely Research Center, 1996.

Petersen, Søren Markkilde. Wind turbine test NORDTANK NTK 500/37 system test. Risø National Laboratory, 1994.

A, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. National Aeronautics and Space Administration, Langley Research Center, 1990.

A, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. National Aeronautics and Space Administration, Langley Research Center, 1990.

A, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. National Aeronautics and Space Administration, Langley Research Center, 1990.

A, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. National Aeronautics and Space Administration, Langley Research Center, 1990.

Kelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. National Aeronautics and Space Administration, Langley Research Center, 1994.

Kelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. National Aeronautics and Space Administration, Langley Research Center, 1994.

K, Abeyounis W., and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. National Aeronautics and Space Administration, Langley Research Center, 1994.