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1

Rudolph, Peter K. C. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

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2

Pittman, 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.

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3

Gatlin, Gregory M. Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations. Hampton, Va: Langley Research Center, 1989.

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4

Hardy, 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.

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5

Mechanical design of high lift systems for high aspect ratio swept wings. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

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6

Mechanical design of high lift systems for high aspect ratio swept wings. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

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7

Center, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

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8

High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

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9

Center, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

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10

Center, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

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11

Noise impact of advanced high lift systems: Contract NAS1-20103. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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12

C, 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.

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13

United 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.

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14

United 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.

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15

1942-, 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.

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16

Radespiel, 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.

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17

(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.

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18

J, 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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