Books on the topic 'Airfoil profiles'

Lye, J. D. Recent developments in augmentor-wing aerofoil sections. [Downsview, Ont.]: De Havilland Aircraft Company of Canada, 1987.

Bousman, William G. Airfoil dynamic stall and rotorcraft maneuverability. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2000.

Allison, Dennis O. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Virginia: National Aeronautics and Space Administration, Langly Research Center, 1996.

Hahne, David E. Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil. Hampton, Va: Langley Research Center, 1991.

Scott, James R. Compressible flows with periodic vortical disturbances around lifting airfoils. [Cleveland, Ohio: Lewis Research Center, 1991.

Johnson, William G. Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Johnson, William G. Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Applin, Zachary T. Pressure distributions from subsonic tests of a NACA 0012 semispan wing model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Applin, Zachary T. Pressure distributions from subsonic tests of a NACA 0012 semispan wing model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Shearin, John G. Acoustic effects on profile drag of a laminar flow airfoil. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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.

Basler, Dieter. Experimentelle Untersuchung der Ausbreitung strossinduzierter Storungen an transsonischen Profilen. Koln: DFVLR, 1987.

Center, Ames Research, ed. Airfoil dynamic stall and rotorcraft maneuverability. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2000.

1934-, Jameson Antony, and Research Institute for Advanced Computer Science (U.S.), eds. A comparison of design variables for control theory based airfoil optimization. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1995.

David, Saunders, and Ames Research Center, eds. PROFILE: Airfoil geometry manipulation and display : user's guide. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

W, Moses Robert, and Langley Research Center, eds. A feasibility study to control airfoil shape using THUNDER. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Improving CPA-TSD steady pressure solutions through airfoil slope modification. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

United States. National Aeronautics and Space Administration., ed. Effect of acoustic excitation on stalled flows over an airfoil. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Center, Ames Research, ed. A two dimensional study of rotor/airfoil interaction in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

1934-, Jameson Antony, and United States. National Aeronautics and Space Administration., eds. Control theory based airfoil design for potential flow and a finite volume discretization. [Washington, DC: National Aeronautics and Space Administration, 1995.

1935-, Lan C. Edward, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Trandesnf: A computer program for transonic airfoil design and analysis in nonuniform flow. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987.

M, Stanislas, and United States. National Aeronautics and Space Administration., eds. Study by double exposure holography of the three-dimensional character of the flow around an airfoil profile in a wind tunnel. Washington, D.C: National Aeronautics and Space Administration, 1986.

Determination of the pressure drag of airfoils by integration of surface pressures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

E, Mineck Raymond, and Langley Research Center, eds. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

E, Mineck Raymond, and Langley Research Center, eds. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

United States. National Aeronautics and Space Administration. and Mississippi State University. Dept. of Aerophysics and Aerospace Engineering., eds. Adaptive grid embedding for the two-dimensional flux-split Euler equations. Mississippi State, Miss: Mississippi State University, Dept. of Aerospace Engineering, 1990.

Control of unsteady separated flow associated with the dynamic stall of airfoils. San Jose, CA: MCAT Institute, 1992.

United States. National Aeronautics and Space Administration., ed. Control of unsteady separated flow associated with the dynamic stall of airfoils: Final report, 95-09. San Jose, CA: MCAT Institute, 1995.

United States. National Aeronautics and Space Administration., ed. Control of unsteady separated flow associated with the dynamic stall of airfoils. San Jose, CA: MCAT Institute, 1994.

In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft). [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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

W, Hicks John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft). [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

W, Hicks John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft). [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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.

A, Garriz Javier, Samareh Jamshid A, and United States. National Aeronautics and Space Administration., eds. The development of a tool for semi-automated generation of structured and unstructured grids about isolated rotorcraft blades. [Washington, D.C: National Aeronautics and Space Administration, 1997.

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. [Washington, DC]: National Aeronautics and Space Administration, 1990.

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. [Washington, DC]: National Aeronautics and Space Administration, 1990.

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Application of a third order upwind scheme to viscous flow over clean and iced wings: 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.

United States. National Aeronautics and Space Administration., ed. Aerodynamics of heat exchangers for high-altitude aircraft. [Washington, DC: National Aeronautics and Space Administration, 1996.

Kyle, Anderson W., Mavriplis Dimitri, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils. [Washington, DC: National Aeronautics and Space Administration, 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.

C, Hall Kenneth, and United States. National Aeronautics and Space Administration., eds. Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades: Final technical report. Durham, NC: Dept. of Mechanical Engineering and Materials Science, School of Engineering, Duke University, 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.

Image processing of aerodynamic data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.