Books on the topic 'Airfoils'

Airfoil selection: Understanding and choosing airfoils for light aircraft. [Irvine, CA]: B. Wainfan, 2005.

Harris, Charles D. NASA supercritical airfoils: a matrix of family-related airfoils. Hampton, Va: Langley Research Center, 1990.

Selig, Michael S. Airfoils at low speeds. Virginia Beach, Va., USA (1504 Horseshoe Cir., Virginia Beach 23451): H.A. Stokely, 1989.

Ray, Edward J. 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, Hampton, Virginia, September 23-27, 1988. Hampton, Va: Langley Research Center, 1989.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Inverse methods for airfoil design for aeronatuical and turbomachinery applications. Neuilly sur Seine, France: AGARD, 1990.

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: NASA, 1985.

Johnston, G. W. Nonlinear unsteady airfoil response studies. [S.l.]: [s.n.], 1989.

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

Barth, Timothy J. Navier-Stokes computations for exotic airfoils. New York: AIAA, 1985.

Alexandris, Georgios. Supersonic flow past two oscillating airfoils. Monterey, Calif: Naval Postgraduate School, 1998.

Davidson, Lars. Predicting stall of a two-dimensional airfoil using an algebraic Reynolds stress model. Toulouse, France: CERFACS, 1991.

Hugues, P. Plantin De. Effect of an extendable slat on the stall behavior of a VR-12 airfoil. Moffett Field, Calif: Ames Research Center, 1993.

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

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

Chan, Y. Y. Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds. Ottawa: National Aeronautical Establishment, National Research Council Canada, 1988.

Center, NASA Glenn Research, ed. Aerodynamic simulation of ice accretion on airfoils. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2011.

Joyce, Richard Kirk. A method of testing two-dimensional airfoils. Monterey, Calif: Naval Postgraduate School, 1992.

Zingg, D. W. Interactive airfoil calculations with higher-order viscous flow equations. Washington, D. C: American Institute of Aeronautics and Astronautics, 1990.

Sudani, Norikazu. Evaluation of NACA0012 airfoil test results in the NAL two-dimensional transonic wind tunnel. Tokyo, Japan: National Aerospace Laboratory, 1991.

Coakley, Thomas J. Numerical simulation of viscous transonic airfoil flows. [Washington, D. C.]: American Institute of Aeronautics and Astronautics, 1987.

Giles, Michael. Non-reflecting boundary conditions for unsteady airfoil calculations. Cambridge, Mass: Massachusetts Institute of Technology, Computational Fluid Dynamics Laboratory, 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.

Mineck, Raymond E. Effect of full-chord porosity on aerodynamic characteristics of the NACA 0012 airfoil. Hampton, Va: Langley Research Center, 1996.

Johnston, G. W. First-order viscous flow predictions with symmetric and aft-loaded airfoils. [S.l.]: [s.n.], 1987.

Zingg, D. W. Interactive airfoil calculations with higher-order viscous-flow equations. Washington, D. C: American Institute of Aeronautics & Astronautics, 1991.

Chang, Jen-Fu. Transonic airfoil analysis and design in nonuniform flow. Hampton, Va: Langley Research Center, 1986.

Poinsatte, Philip E. Heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Icing Research Tunnel. Cleveland, Ohio: Lewis Research Center, 1990.

Dovgal, Alexander. Control of leading-edge separation on an airfoil by localized excitation. Koln: DLR, 1993.

Hirose, Naoki. Computational and experimental research on buffet phenomena of transonic airfoils. Tokyo: National Aerospace Laboratory, 1988.

Rodman, L. C. Verification of performance results for a low-speed 15% elliptical circulation control airfoil. Stanford, Calif: Stanford University, Dept. of Aeronautics and Astronautics, 1986.

Venkatakrishnan, V. Newton solution of inviscid and viscous problems. New York: AIAA, 1988.

Lee, B. H. K. Flutter analysis of a two-dimensional airfoil with cubic non-linear restoring force. Ottawa: National Aeronautical Establishment, 1986.

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.

L, Ladson Charles, and Langley Research Center, eds. Computer program to obtain ordinates for NACA airfoils. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Stewart, Mark E. M. Non-overlapping composite meshes for multi-element airfoils. Princeton, N. J: Princeton University, 1990.

Center, NASA Glenn Research, ed. Ice accretions and icing effects for modern airfoils. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2000.

Venkatakrishnan, V. Computation of unsteady transonic flows over moving airfoils. Princeton, N.J: Princeton University, 1987.

L, Ladson Charles, and Langley Research Center, eds. Computer program to obtain ordinates for NACA airfoils. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

D, Salas M., and United States. National Aeronautics and Space Administration., eds. Optimum transonic airfoils based on the Euler equations. [Washington, DC: National Aeronautics and Space Administration, 1997.

Chʻung-lung, Chʻen, and Ames Research Center, eds. Numerical study of porous airfoils in transonic flow. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

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.

L, Cross Jeffrey, Noonan Kevin W, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Modi, V. J. Moving surface boundary-layer control as applied to two-dimensional airfoils. New York: AIAA, 1989.

Anderson, W. Kyle. Navier-Stokes computations and experimental comparisons for multielement airfoil configurations. Washington, D. C: American Institute of Aeronautics and Astronautics, 1993.

United States. National Aeronautics and Space Administration., ed. Evaluation of constant-Weber-number scaling for icing tests. [Washington, DC]: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Evaluation of constant-Weber-number scaling for icing tests. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Khalid, M. Use of riblets to obtain drag reduction on airfoils at high Reynolds number flows. Ottawa: National Aeronautical Establishment, National Research Council Canada, 1988.

Kozel, Karel. Numerical simulation of two-dimensional transonic flow over thin oscillating airfoil. Praha, Czechoslovakia: Information Centre for Aeronautics, 1986.

Sudani, Norikazu. A comparative study of BGK No. 1 airfoil data in high Reynolds number transonic wind tunnels. Tokyo: National Aerospace Laboratory, 1993.

L, Cross Jeffrey, Noonan Kevin W, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.