Books on the topic 'Aerofoil'

Melocco, F. Computational method for high-lift aerofoil flows. Manchester: UMIST, 1995.

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

Papastavrou, P. Prediction of transition for high lift aerofoil systems. Manchester: UMIST, 1996.

Muhoho, A. P. Transonic Aerofoil computations using Grid Navier-Stokes Solver. Manchester: UMIST, 1996.

Fulker, J. L. Validation of cfd methods for transonic aerofoil and wing flows. London: HMSO, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Aerofoil testing in a self-streamlining flexible walled wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Moir, I. R. M. Measurements on a two-dimensional aerofoil with high-lift devices. Farnborough: Defence Research Agency, 1994.

Fulker, J. L. Study of simulated active control of shock waves on an aerofoil. Farnborough: Defence Research Agency, 1993.

The enigma of the aerofoil: Rival theories in aerodynamics, 1909-1930. Chicago: The University of Chicago Press, 2011.

Ashill, P. R. A novel technique for controlling shock strength of laminar-flow aerofoil sections. Farnborough: Defence Research Agency, 1993.

Ashill, P. R. Wind tunnel experiments on aerofoil models for the assessment of computational flow methods. London: HMSO, 1988.

Taki, Mustafa. Computation of the aerodynamic performance of high-lift aerofoil systems at low-speed and transonic flow conditions. Manchester: UMIST, 1997.

McDonald, M. A. Measurements and analysis of the mean shear-layer flow over the RAE 2822 aerofoil at 28 degrees sweep and at subsonicspeeds. London: HMSO, 1989.

Vila, Ana María Ruiz. Aerofoto. Edited by Fundación ICA and Foto Museo Cuatro Caminos. Ciudad de México: Fundación ICA, 2017.

Lynn, Tylczak, and Koda Harold, eds. Česká republika: Aerofoto. 2nd ed. Praha: Kvarta, 2004.

Mueller, T. J. The structure of separated flow regions occuring near the leading edge of airfoils including transition. [Washington, DC: National Aeronautics and Space Administration, 1987.

Srinivasan, G. Computations of two-dimensional airfoil-vortex interactions. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

M, Russell Louis, Torres Felix J, and United States. National Aeronautics and Space Administration., eds. Use of a liquid-crystal, heater-element composite for quantitative, high-resolution heat transfer coefficients on a turbine airfoil, including turbulence and surface roughness effects. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

1936-, Tung C., and Ames Research Center, eds. Suppression of dynamic stall with a leading-edge slat on a VR-7 airfoil. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Technology for pressure-instrumented thin airfoil models. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

M, Russell Louis, Torres Felix J, and United States. National Aeronautics and Space Administration., eds. Use of a liquid-crystal, heater-element composite for quantitative, high-resolution heat transfer coefficients on a turbine airfoil, including turbulence and surface roughness effects. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

J, Berchak M., and United States. National Aeronautics and Space Administration., eds. Two-dimensional aerodynamic characteristics of the Ames HI-120, HI-8, and LOW-12 airfoils. Columbus, Ohio: The Ohio State University, Aeronautical and Astronautical Research Laboratory, 1987.

J, Berchak M., and United States. National Aeronautics and Space Administration., eds. Two-dimensional aerodynamic characteristics of the Ames HI-120, HI-8, and LOW-12 airfoils. Columbus, Ohio: The Ohio State University, Aeronautical and Astronautical Research Laboratory, 1987.

Wigley, D. A. Technology for pressure-instrumented thin airfoil models. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Srinivasan, G. Computations of two-dimensional airfoil-vortex interactions. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

M, Russell Louis, Torres Felix J, and United States. National Aeronautics and Space Administration., eds. Use of a liquid-crystal, heater-element composite for quantitative, high-resolution heat transfer coefficients on a turbine airfoil, including turbulence and surface roughness effects. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

M, Russell Louis, Torres Felix J, and United States. National Aeronautics and Space Administration., eds. Use of a liquid-crystal, heater-element composite for quantitative, high-resolution heat transfer coefficients on a turbine airfoil, including turbulence and surface roughness effects. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

Wigley, D. A. Technology for pressure-instrumented thin airfoil models. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

United States. National Aeronautics and Space Administration., ed. Final report for modeling of heavy-gas effects on airfoil flows. [Washington, DC: National Aeronautics and Space Administration, 1992.

Airfoil design and data. Berlin: Springer-Verlag, 1990.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Inviscid analysis of two supercritical laminar-flow-control airfoils at design and off-design conditions. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

J, Betts C. Comparison of calculation and experiment for three thick aerofoils. London: HMSO, 1990.

Cook, Robert Manuel. Airfoil Vibration Dampers Program, contract no. NAS8-36720: Final report. [Washington, DC: National Aeronautics and Space Administration, 1991.

Nicks, Oran W. Experimental verification of a new laminar airfoil: A project for the graduate program in aeronautics : final report. [College Station, Tex.]: Texas A&M University, Aerospace Engineering Dept., 1991.

K. B. M. Q. Zaman. A natural low frequency oscillation in the wake of an airfoil near stalling conditions. [Washington, DC]: National Aeronautics and Space Administration, 1988.

J, Kuniega R., Nyland Ted W, United States. Dept. of Energy. Wind/Ocean Technologies Division., and United States. National Aeronautics and Space Administration., eds. Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application. Washington, D.C: U.S. Dept. of Energy, Conservation and Renewable Energy, Wind/Ocean Technology Division, 1988.

Rishi, Raj, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. An investigation of the flow characteristics in the blade endwall corner region. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Ferris, James C. Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil. Hampton, Va: Langley Research Center, 1987.

Barnett, M. An analysis of the crossover between local and massive separation on airfoils. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

W, Rubesin Morris, MacCormack R. W. 1940-, and Ames Research Center, eds. On the validation of a code and a turbulence model appropriate to circulation control airfoils. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

United States. National Aeronautics and Space Administration., ed. Icing characteristics of a natural-laminar-flow, a medium-speed, and a swept,medium-speed airfoil. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Cole, Gregory M. Experimental measurements of the laminar separation bubble on an Eppler 387 airfoil at low Reynolds numbers: Final report. Notre Dame, Ind: Aerodynamics Laboratory, Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1990.

J, Wood N., and Ames Research Center, eds. Verification of performance results for a low-speed 15% eliptical circulation control airfoil. Stanford, Calif: Joint Institute for Aeronautics and Acoustics, 1986.

E, Mineck Raymond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

G, Meyer T., Walker K. P, and United States. National Aeronautics and Space Administration., eds. Life prediction and constitutive models for engine hot section anisotropic materials program: Final report. [Washington, DC: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Maurice, Holt. Supercritical flow past a symmetrical bicircular arc airfoil. Berkeley, CA: Dept. of Mechanical Engineering, University of California, 1989.

Stuart, Pope D., Marcolini Michael A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, eds. Airfoil self-noise and prediction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Stuart, Pope D., Marcolini Michael A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, eds. Airfoil self-noise and prediction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Rishi, Raj, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. An investigation of the flow characteristics in the blade endwall corner region. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.