Books on the topic 'Wings – Mathematical models'

Teorii͡a nesushcheĭ poverkhnosti: Matematicheskai͡a modelʹ, chislennyĭ metod, raschet mashushchego poleta. Moskva: Nauka, Fizmatlit, 1995.

Bina, Bardia. Wing anti-icing system control modelling and sensitivity analysis: A system identification based approach. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.

Turk, Thomas Andrew. Aircraft wing anti-icing system: Modelling, integration, and validation. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.

Powell, Kenneth G. Vortical solutions of the conical Euler equations. Braunschweig: Vieweg, 1990.

Hollowell, S. J. Conceptual design optimization study. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Klein, Thomas. Katabatic winds over Greenland and Antarctica and their interaction with mesoscale and synoptic scale weather systems: Investigations using three dimensional numerical models. St. Augustin: Asgard, 2000.

Wuertz, David B. Editing wind profiler measurements. Boulder, Colo: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Wave Propagation Laboratory, 1989.

Wuertz, David B. Editing wind profiler measurements. Boulder, Colo: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Wave Propagation Laboratory, 1989.

Wuertz, David B. Editing wind profiler measurements. Boulder, Colo: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Wave Propagation Laboratory, 1989.

Klaus, Braun. Der Einfluss mesoskaliger Windfelder auf die räumliche Verteilung des Niederschlags: Eine Untersuchung zur Regionalisierung von Niederschlagsdaten mit Hilfe eines mesoskaligen Strömungsmodells. Freiburg: Im Selbstverlag des Institutes für Physische Geographie der Albert-Ludwigs-Universität Freiburg i. Br., 1997.

Phillips, James D. Modal control of an oblique wing aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Schuhmacher, Peter. Messung und numerische Modellierung des Windfeldes über einer Stadt in komplexer Topographie. Zürich: Verlag der Fachvereine Zürich, 1992.

Schwenzfeger, K. J. Comparison of ERS-1 scatterometer Monte Carlo performance simulations using a weighted nonlinear least-squares and a maximum likelihood estimation method. Neubiberg: Hochschule der Bundeswehr München, 1985.

Kamada, Ray. Preliminary review of flow models considered for use at Vandenberg Air Force Base. Monterey, Calif: Naval Postgraduate School, 1989.

Rennick, Mary Alice. Solutions to the shallow water equations in an ocean basin forced by unsteady winds. Monterey, Calif: Naval Postgraduate School, 1988.

Justus, C. G. The NASA/MSFC global reference atmospheric model--1990 version (GRAM-90). Atlanta, Ga: School of Earth and Atmospheric Sciences, Georgia Institue of Technology, 1990.

Schwenzfeger, K. J. Auswertung von gemessenen Rückstreukoeffizienten im Hinblick auf bestehende Windfelder. Neubiberg: Universität der Bundeswehr München, 1985.

Lanicci, John M. Sensitivity tests of a surface-layer windflow model to effects of stability and vegetation. Hanscom AFB, MA: Atmospheric Sciences Division, Air Force Geophysics Laboratory, 1985.

Brainard, S. Lael. Last one out wins: Trade policy in an international exit game. Cambridge, MA: National Bureau of Economic Research, 1990.

Russell, Sarah L. Shelf currents, ice and wind: A numeric modeling study. Cambridge, Mass: Massachusetts Institute of Technology, 2003.

Goretzki, Bernd. Untersuchungen zur Ausbreitung und Entwicklung von Rossby-Wellen in einem dreidimensionalen, globalen numerischen Modell bei Anwesenheit einer subtropischen kritischen Schicht. Berlin: D. Reimer, 1988.

Zdunich, Patrick. A discrete vortex model of unsteady separated flow about a thin airfoil for application to hovering flapping-wing flight. Ottawa: National Library of Canada, 2002.

Zdunich, Patrick. A discrete vortex model of unsteady separated flow about a thin airfoil for application to hovering flapping-wing flight. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2002.

Maarouf, A. Windchill indices : a review of science, current applications and future directions for Canada =: Indices de refroidissement éolien : examen de la science, des applications actuelles et des orientations futures pour le Canada. Downsview, Ont: Meteorological Service of Canada, Environment Canada = Service météorologique du Canada, Environnement Canada, 2000.

Kamada, Ray. A comparison of eight cases selected from the vandenberg AFB Mt. Iron tracer study with results from the Lincoln/Rimpuff dispersion model. Monterey, Calif: Naval Postgraduate School, 1991.

Craig, Ken. Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings. Stanford, Calif: Stanford University, Dept. of Aeronautics and Astronautics, 1991.

Craig, Ken. Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings. Stanford, Calif: Stanford University, Dept. of Aeronautics and Astronautics, 1991.

NATO Advanced Research Workshop "Atmospheric Boundary Layers: Modelling and Applications to Environmental Security" (2006 Dubrovnik, Croatia). Atmospheric boundary layers: Nature, theory, and application to environmental modelling and security. Edited by Baklanov Alexander and Grisogono B. New York: Springer Science+Business Media, 2007.

Lin, Yuh-Lang. Numerical modeling studies of wake vortex transport and evolution within the planetary boundary layer: FY94 July semi-annual report. Raleigh, NC: Dept. of Marine, Earth and Atmospheric Sciences, North Carolina State University, 1994.

Pierson, Willard J. Probabilities and statistics for backscatter estimates obtained by a scatterometer with applications to new scatterometer design data. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

K, Brown Christopher, and United States. National Aeronautics and Space Administration., eds. Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests: Final report. Morgantown, WV: West Virginia University, Mechanical and Aerospace Engineering Dept., 1989.

Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

K, Brown Christopher, and Langley Research Center, eds. Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests. Morgantown, WV: Mechanical and Aerospace Engineering Dept., West Virginia University, 1988.

Center, Ames Research, ed. Theoretical studies on flapped delta wings. [Moffett Field, Calif.]: National Aeronautics and Space Administration, Ames Research Center, 1988.

Center, Langley Research, ed. Numerical simulation of swept-wing flows: A progress report for graduate program in aeronautics. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Numerical simulation of swept-wing flows: A progress report for graduate program in aeronautics. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Smetana, Frederick O. Introductory Aerodynamics and Hydrodynamics of Wings and Bodies: A Software-Based Approach (Aiaa Education Series). AIAA (American Institute of Aeronautics & Ast, 1997.

United States. National Aeronautics and Space Administration., ed. A numerical model of unsteady, subsonic aeroelastic behavior. [Washington, D.C: National Aeronautics and Space Administration, 1987.

Center, Langley Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Nonlinear aerodynamic wing design. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

1945-, Bennett Robert M., and Langley Research Center, eds. Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Center, Langley Research, ed. A parametric study of accelerations of an airplane due to a wake vortex system. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

A new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.

A new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. A new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. A new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.

The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

H, Hoffmann P., and Joint Institute for Aeronautics and Acoustics., eds. A study of the factors affecting boundary layer two-dimensionality in wind tunnels. Stanford, CA: Stanford University, Dept. of Aeronautics and Astronautics, 1986.

E, Fortin Paul, and United States. National Aeronautics and Space Administration., eds. An integrated study of structures, aerodynamics, and controls on the forward swept wing X-29A and the oblique wing research aircraft. Lawrence, Kan: University of Kansas, Center for Research, 1987.

Center, Langley Research, ed. Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Full potential methods for analysis/design of complex aerospace configurations. Los Angeles, Calif: Rockwell International Corp., 1986.