Libros sobre el tema "Airplanes, Tailless. Airplanes Fluid dynamics"

Korus, Andreas. Experimentelle und theoretische Untersuchungen über den Strahleinfluss bei der Umströmung eines Bypass-Triebwerkes. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1993.

Garodz, Leo J. Vortex characteristics of C5A/B, C141B, and C130E aircraft applicable to ATC terminal flight operations tower fly-by data. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Air Resources Laboratory, 1991.

Yahya, S. M. Fundamentals of compressible flow: SI units with aircraft and rocket propulsion. 3^a ed. New Delhi: New Age International, 2003.

1962-, Breitsamter Christian, ed. New results in numerical and experimental fluid mechanics IV: Contributions to the 13th STAB/DGLR Symposium, München, Germany 2002. Berlin: Springer-Verlag, 2004.

Fejtek, Ian G. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Washington, D. C: Ames Research Center, 1993.

AG, STAB/DGLR Symposium (10th 1996 Braunschweig Germany). New results in numerical and experimental fluid mechanics: Contributions to the 10th AG STAB/DGLR Symposium, Braunschweig, Germany 1996. Braunschweig/Wiesbaden: Vieweg, 1997.

Ing, Wagner Siegfried Dr, ed. New results in numerical and experimental fluid mechanics III: Contributions to the 12th STAB/DGLR symposium, Stuttgart, Germany, 2000. Berlin: Springer, 2002.

1954-, Tropea Cameron, Arbeitsgemeinschaft Strömungen mit Ablösung y Deutsche Gesellschaft für Luft- und Raumfahrt., eds. New results in numerical and experimental fluid mechanics VI: Contributions to the 15th STAB/DGLR Symposium, Darmstadt, Germany, 2006. Berlin: Springer, 2007.

AG, STAB/DGLR Symposium (11th 1998 Berlin Germany). New results in numerical and experimental fluid mechanics II: Contributions to the 11th AG STAB/DGLR Symposium, Berlin, Germany 1998. Braunschweig/Wiesbaden: Vieweg, 1999.

Dillmann, Andreas. New Results in Numerical and Experimental Fluid Mechanics VII: Contributions to the 16th STAB/DGLR Symposium Aachen, Germany 2008. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010.

Schwartzentruber, Thomas. Suppression of premature ignition in the pre-mixed inlet flow of a shcramjet. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Specialists' Meeting. Effects of adverse weather on aerodynamics: Papers presented and discussions held at the Fluid Dynamics Panel Specialists' Meeting held in Toulouse, France, 29th April - 1st May 1991 = Les effets des conditions météorologiques adverses sur l'aérodynamique. Neuilly sur Seine, France: Advisory Group for Aerospace Research & Development, 1991.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of 3-D aircraft afterbodies. Neuilly-sur-Seine: AGARD, 1995.

Fluid dynamics research on supersonic aircraft =: Les travaux de recherche en dynamique des fluides relatifs aux aéronefs supersoniques. [Neuilly-sur-Seine Cedex, France: North Atlantic Treaty Organization, Research and Technology Organization, 1998.

Joint Symposium of the Fluid Dynamics and Flight Mechanics Panels (1985 Göttingen, Germany). Unsteady aerodynamics, fundamentals and applications to aircraft dynamics: Papers presented and discussions held at the Joint Symposium of the Fluid Dynamics and Flight Mechanics Panels held in Göttingen, Federal Republic of Germany, 6-9 May 1985. Neuilly sur Seine, France: Advisory Group for Aerospace Research & Development, 1985.

Wolf, D. E. Fully-coupled analysis of jet mixing problems: Three-dimensional PNS model, SCIP3D. Hampton, Va: Langley Research Center, 1988.

Wolf, D. E. Fully-coupled analysis of jet mixing problems: Three-dimensional PNS model, SCIP3D. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

STAB/DGLR Symposium (14th 2004 Bremen, Germany). New results in numerical and experimental fluid mechanics V: Contributions to the 14th STAB/DGLR Symposium, Bremen, Germany, 2004. Editado por Breitsamter Christian 1962-. Berlin: Springer-Verlag, 2006.

Chaffin, Mark S. Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment. Hampton, Va: Langley Research Center, 1994.

My reproductive research: Insights into the control systems that work inside us and in our world. Brighton: Book Guild Publishing, 2007.

Kuruvila, G. Three-dimensional simulation of vortex breakdown. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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.

Imlay, Scott T. Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows. Hampton, Va: Langley Research Center, 1986.

Hahne, David E. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Holland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

M, Richwine David, Banks Daniel W y Dryden Flight Research Facility, eds. Surface flow visualization of separated flows on the forebody of an F-18 aircraft and wind-tunnel model. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.

United States. National Aeronautics and Space Administration., ed. A two-dimensional Euler solution for an unbladed jet engine configuration. [Washington, DC]: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. A two-dimensional Euler solution for an unbladed jet engine configuration. [Washington, DC]: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. Physics of forebody flow control. San Jose, CA: MCAT Institute, 1993.

United States. National Aeronautics and Space Administration., ed. Physics of forebody flow control. San Jose, CA: MCAT Institute, 1993.

United States. National Aeronautics and Space Administration., ed. Computation technique for compressible vortex flows using the integral equation solution: Final report. Norfolk, Va: Dept. of Mechanical Engineering and Mechanics, College of Engineering, Old Dominion University, 1988.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of the reactive flow in advanced (HSR) combustors using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of the reactive flow in advanced (HSR) combustors using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1991.

(Editor), Christian Breitsamter, Boris Laschka (Editor), Hans-Joachim Heinemann (Editor) y Reinhard Hilbig (Editor), eds. New Results in Numerical and Experimental Fluid Mechanics IV: Contributions to the 13th STAB/DGLR Symposium Munich, Germany 2002 (Notes on Numerical Fluid ... and Multidisciplinary Design (NNFM)). Springer, 2004.

New Results in Numerical and Experimental Fluid Mechanics III (Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)). Springer, 2002.

Vortex characteristics of C5A/B, C141B and C130E aircraft applicable to ATC terminal flight operations tower fly-by data. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Air Resources Laboratory, 1991.

L, Clawson K. y Air Resources Laboratory (U.S.), eds. Vortex characteristics of C5A/B, C141B and C130E aircraft applicable to ATC terminal flight operations tower fly-by data. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Air Resources Laboratory, 1991.

Gidrogazodinamika i teplomassoobmen letatelʹnykh apparatov: Sbornik nauchnykh trudov. Kiev: Nauk. dumka, 1988.

Behavior of turbulent gas jets in an axisymmetric confinement. [Washington, DC: National Aeronautics and Space Administration, 1985.

Center, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

Dmitrievich, Kovalenko Nikolaĭ y Institut tekhnicheskoĭ mekhaniki (Akademii͡a︡ nauk Ukraïnsʹkoï RSR), eds. Nestat͡s︡ionarnye teplovye prot͡s︡essy v ėnergeticheskikh ustanovkakh letatelʹnykh apparatov. Kiev: Nauk. dumka, 1988.

Center, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

Dinamika uprugogazozhidkostnykh sistem pri vibrat͡s︡ionnykh vozdeĭstvii͡a︡kh. Kiev: Nauk. dumka, 1988.

Center, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

Schröder, Wolfgang, Hans-Peter Kreplin, Andreas Dillmann, Michael Klaas, Gerd Heller y Wolfgang Nitsche. New Results in Numerical and Experimental Fluid Mechanics VII: Contributions to the 16th STAB/DGLR Symposium Aachen, Germany 2008. Springer, 2014.

Schröder, Wolfgang, Andreas Dillmann y Gerd Heller. New Results in Numerical and Experimental Fluid Mechanics VII: Contributions to the 16th STAB/DGLR Symposium Aachen, Germany 2008. Springer, 2011.

Progress and challenges in CFD methods and algorithms =: Progrès réalisés et défis en méthodes et algorithmes CFD. Neuilly-sur-Seine: North Atlantic Treaty Organization, 1996.

Fluid dynamics research on supersonic aircraft =: Les travaux de recherche en dynamique des fluides relatifs aux aeronefs supersoniques (RTO educational notes). [NASA Center for Aerospace Information, distributor], 1998.

Ihab, Adam, Wong Tin Chee, American Institute of Aeronautics and Astronautics. y United States. National Aeronautics and Space Administration., eds. Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes: 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.

Ihab, Adam, Wong Tin Chee, American Institute of Aeronautics and Astronautics. y United States. National Aeronautics and Space Administration., eds. Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes: 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA. Washington, DC: American Institute of Aeronautics and Astronautics, 1996.