Books on the topic 'High-lift airfoil'

Valarezo, Walter O. Multi-element airfoil optimization for maximum lift at high Reynolds numbers. New York: American Institute of Aeronautics and Astronautics, 1991.

Davidson, Lars, Davor Cokljat, Jochen Fröhlich, Michael A. Leschziner, Chris Mellen, and Wolfgang Rodi, eds. LESFOIL: Large Eddy Simulation of Flow Around a High Lift Airfoil. Berlin, Heidelberg: Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-540-36457-3.

Applin, Zachary T. Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Pfenninger, Werner. Optimization of natural laminar flow airfoils for high section lift-to-drag ratios in the lower Reynolds number range. Washington, D. C: AIAA, 1989.

Morgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.

Morgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.

Morgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.

Fisher, David. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. [Washington, DC: National Aeronautics and Space Administration, 1996.

Fisher, David. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. [Washington, DC: National Aeronautics and Space Administration, 1996.

Godin, Philippe. Turbulence modeling for high-lift multi-element airfoil configurations. 2004.

Lee, Hee W. Contributions to the analysis of high-lift airfoil aerodynamics. 1986.

Valarezo, Walter O. Multi-element airfoil optimization for maximum lift at high Reynolds numbers. 1991.

The effect of heavy rain on an airfoil at high lift. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Nelson, Thomas Edward. Numerical solution of the Navier-Stokes equations for high-lift airfoil configurations. 1994.

R, Miller Dean, United States. National Aeronautics and Space Administration., and Lewis Research Center, eds. Further investigations of icing effects on an advanced high-lift multi-element airfoil. [Washington, DC]: National Aeronautics and Space Administration, 1995.

R, Miller Dean, and United States. National Aeronautics and Space Administration., eds. Further investigations of icing effects on an advanced high-lift multi-element airfoil. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Jaiwon, Shin, and United States. National Aeronautics and Space Administration., eds. Icing test results on an advanced two-dimensional high-lift multi-element airfoil. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Comparative results from a CFD challenge over a 2D three-element high-lift airfoil. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

J, McGhee Robert, and Langley Research Center, eds. Experimental results for a flapped natural-laminar-flow airfoil with high lift/drag ratio. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

C, Ostowari, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Additional flow field studies of the GA(W)-1 airfoil with 30-percent chord Fowler flap including slot-gap variations and cove shape modifications. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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.

Lars, Davidson, ed. LESFOIL: Large eddy simulation of flow around a high lift airfoil : results of the Project LESFOIL supported by the European Union, 1998-2001. Berlin: Springer, 2003.

Rodi, Wolfgang, Lars Davidson, Chris Mellen, Davor Cokljat, Jochen Fronlich, and Micheal A. Leschziner. LESFOIL : Large Eddy Simulation of Flow Around a High Lift Airfoil: Results of the Project LESFOIL Supported by the European Union 1998 - 2001. Springer Berlin Heidelberg, 2010.

P, Van Dam C., and United States. National Aeronautics and Space Administration., eds. Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data: Final report. Davis, CA: Dept. of Mechanical and Aeronautical Engineering, University of California, 1995.

P, Van Dam C., and United States. National Aeronautics and Space Administration., eds. Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data: Final report. Davis, CA: Dept. of Mechanical and Aeronautical Engineering, University of California, 1995.

P, Van Dam C., and United States. National Aeronautics and Space Administration., eds. Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data: Final report. Davis, CA: Dept. of Mechanical and Aeronautical Engineering, University of California, 1995.

(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.

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.

Center, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Center, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Center, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Center, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

O, Thomas Flint, Nelson Robert C, and United States. National Aeronautics and Space Administration., eds. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. [Washington, DC: National Aeronautics and Space Administration, 1996.

O, Thomas Flint, Nelson Robert C, and United States. National Aeronautics and Space Administration., eds. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. [Washington, DC: National Aeronautics and Space Administration, 1996.