Books on the topic 'Aerofoils'

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.

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.

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.

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

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

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.

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.

Althoff, Susan L. Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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.

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.

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

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.

Othman, Ashraf. Feasibility study for a floatwing waterborne aircraft type. Ottawa: National Library of Canada, 2001.

M, Gregorek G., and United States. National Aeronautics and Space Administration., eds. Wind tunnel evaluation of a truncated NACA 64-621 airfoil for wind turbine applications. [Washington, DC: National Aeronautics and Space Administration, 1987.

Thomas, Stengle, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Flight Mechanics/Estimation Theory Symposium, 1989: Proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

P, Proctor Margaret, and United States. National Aeronautics and Space Administration., eds. Transient technique for measuring heat transfer coefficients on stator airfoils in a jet engine environment. [Washington, DC: National Aeronautics and Space Administration, 1985.

CAST-10-2/DOA 2 Airfoil Studies Workshop (1988 NASA Langley Research Center). CAST-10-2/DOA 2 Airfoil Studies Workshop results: Proceedings of a workshop. Washington, D.C: NASA, Office of Management, Scientific and Technical Information Division, 1989.

United States. National Aeronautics and Space Administration., ed. Oscillating airfoils and their wake. Washington DC: National Aeronautics and Space Administration, 1986.

S, Walker Betty, Millard Betty F, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

W, Nicks Oran, Heffner Michael, and United States. National Aeronautics and Space Administration., eds. Further wind tunnel investigation of the SM701 airfoil with aileron and turbulators. College Station, Tex: [Texas A&M University, 1992.

H, Snyder M., and Langley Research Center, eds. Calibration of averaging total pressure flight wake rake and natural-laminar-flow airfoil drag certification. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

J, Ray Edward, Hill Acquilla S, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. CAST-10-2/DOA 2 Airfoil Studies Workshop results: Proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at NASA Langley Research Center, Hamnpton, Virginia, September 23-27, 1988. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Othman, Ashraf. Feasibility study for a floatwing waterborne aircraft type. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2001.

Krasilʹshchikova, E. A. Tonkoe krylo v szhimaemom potoke. 2nd ed. Moskva: "Nauka," Glav. red. fiziko-matematicheskoĭ lit-ry, 1986.

Lan, C. Edward. Applied airfoil and wing theory. Taipei, Taiwan, Republic of China (20 Heng Yang Rd., Taipei): Cheng Chung Book Co., 1988.

Ahmed, S. Numerical computation of viscous flow about unconventional airfoil shapes: Final report. Ames, Iowa: Engineering Research Institute, 1990.

1952-, Panda Jagannath, Rumsey Christopher Lockwood, and United States. National Aeronautics and Space Administration., eds. Estimation of unsteady lift on a pitching airfoil from wake velocity surveys. [Washington, DC: National Aeronautics and Space Administration, 1993.