Books on the topic 'High-lift design'
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Rudolph, Peter K. C. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textPittman, Jimmy L. Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textGatlin, Gregory M. Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations. Hampton, Va: Langley Research Center, 1989.
Find full textHardy, B. C. The aerodynamic design of a model for the RAE 5m wind tunnel to investigate scale effects at low speed and high lift. London: HMSO, 1991.
Find full textMechanical design of high lift systems for high aspect ratio swept wings. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Find full textMechanical design of high lift systems for high aspect ratio swept wings. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Find full textCenter, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textHigh-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textCenter, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textCenter, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textNoise impact of advanced high lift systems: Contract NAS1-20103. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textC, Joshi Mahendra, and Langley Research Center, eds. Noise impact of advanced high lift systems: Contract NAS1-20103. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full text1942-, Nelson Robert C., and United States. National Aeronautics and Space Administration., eds. Annual progress report ... entitled An experimental investigation of the flow physics of high-lift systems, for the period March-December 1995. 2nd ed. [Washington, DC: National Aeronautics and Space Administration, 1995.
Find full textRadespiel, Rolf, and Richard Semaan. Fundamentals of High Lift for Future Civil Aircraft: Contributions to the Final Symposium of the Collaborative Research Center 880, December 17-18, ... Mechanics and Multidisciplinary Design ). Springer, 2020.
Find full text(Editor), Lars Davidson, Davor Cokljat (Editor), Jochen Fröhlich (Editor), Michael A. Leschziner (Editor), Chris Mellen (Editor), and Wolfgang Rodi (Editor), eds. LESFOIL: Large Eddy Simulation of Flow Around a High Lift Airfoil: Results of the Project LESFOIL Supported by the European Union 1998 - 2001 (Notes on ... and Multidisciplinary Design (NNFM)). Springer, 2003.
Find full textJ, Dominik C., American Institute of Aeronautics and Astronautics., and AIAA Applied Aerodynamics Conference (13th : 1995 : San Diego, Calif.).), eds. Optimization of an advanced design three-element airfoil at high reynolds numbers. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.
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