Books on the topic 'Drag reduction'
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Thiede, Peter, ed. Aerodynamic Drag Reduction Technologies. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-540-45359-8.
Full textSchaus, Ph. Viscous drag reduction of horizontal plates. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1987.
Find full textLi, Feng-Chen, Bo Yu, Jin-Jia Wei, and Yasuo Kawaguchi. Turbulent Drag Reduction by Surfactant Additives. Singapore: John Wiley & Sons Singapore Pte. Ltd., 2011. http://dx.doi.org/10.1002/9781118181096.
Full textGyr, Albert, ed. Structure of Turbulence and Drag Reduction. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-50971-1.
Full textLi, Feng-Chen. Turbulent drag reduction by surfactant additives. Hoboken, N.J: Wiley, 2011.
Find full textM, Bushnell Dennis, and Hefner Jerry M, eds. Viscous drag reduction in boundary layers. Washington, DC: American Institute of Aeronautics and Astronautics, 1990.
Find full textDam, R. F. van den. SAMID, an interactive system for aircraft drag minimization studies (mathematical models and methods). Amsterdam, Netherlands: National Aerospace Laboratory, 1988.
Find full textGyr, A., and H. W. Bewersdorff. Drag Reduction of Turbulent Flows by Additives. Dordrecht: Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-017-1295-8.
Full textStanewsky, Egon, Jean Délery, John Fulker, and Wolfgang Geißler, eds. EUROSHOCK - Drag Reduction by Passive Shock Control. Wiesbaden: Vieweg+Teubner Verlag, 1997. http://dx.doi.org/10.1007/978-3-322-90711-0.
Full textGyr, A. Drag Reduction of Turbulent Flows by Additives. Dordrecht: Springer Netherlands, 1995.
Find full textAdvisory Group for Aerospace Research and Development. Fluid Dynamics Panel., ed. Special course on skin friction drag reduction. Neuilly sur Seine: Agard, 1992.
Find full text-W, Bewersdorff H., ed. Drag reduction of turbulent flows by additives. Dordrecht: Kluwer Academic, 1995.
Find full textSmith, Leigh Ann. Effects of winglets on the drag of a low-aspect-ratio configuration. Hampton, Va: Langley Research Center, 1996.
Find full textSmith, Leigh Ann. Effects of winglets on the drag of a low-aspect-ratio configuration. Washington, DC: National Aeronautics and Space Administration, 1996.
Find full textSlooff, J. W. Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible? Neuilly sur Seine, France: AGARD, 1986.
Find full textCEAS/DragNet European Drag Reduction Conference (2000 Potsdam, Germany). Aerodynamic drag reduction technologies: Proceedings of the CEAS/DragNet European Drag Reduction Conference, 19-21 June 2000, Potsdam, Germany. Edited by Thiede Peter 1938-. Berlin: Springer, 2001.
Find full textCEAS/DragNet European Drag Reduction Conference (2000 Potsdam, Germany). Aerodynamic drag reduction technologies: Proceedings of the CEAS/DragNet European Drag Reduction Conference, 19-21 June 2000, Potsdam, Germany. Berlin: Springer, 2001.
Find full textStanewsky, Egon, Jean Délery, John Fulker, and Paolo Matteis, eds. Drag Reduction by Shock and Boundary Layer Control. Berlin, Heidelberg: Springer Berlin Heidelberg, 2002. http://dx.doi.org/10.1007/978-3-540-45856-2.
Full textKhalid, M. Use of riblets to obtain drag reduction on airfoils at high Reynolds number flows. Ottawa: National Aeronautical Establishment, National Research Council Canada, 1988.
Find full textUnited States. National Aeronautics and Space Administration., ed. Viscous flow drag reduction by acoustic excitation: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1987.
Find full textJ, Sellin Robert H., Moses R. T, and International Conference on Drag Reduction (4th : 1989 : Davos, Switzerland), eds. Drag reduction in fluid flows: Techniques for friction control. Chichester: Published for the International Association for Hydraulic Research by E. Horwood, 1989.
Find full textStephanie, Sprague, Naughton Jonathan W. 1964-, and Hugh L. Dryden Flight Research Center., eds. Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2001.
Find full textStephanie, Sprague, Naughton Jonathan W. 1964-, and Hugh L. Dryden Flight Research Center., eds. Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2001.
Find full textStephanie, Sprague, Naughton Jonathan W. 1964-, and Hugh L. Dryden Flight Research Center., eds. Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2001.
Find full textKrogmann, Paul. Untersuchungen an einem transsonischen Profil mit 30 mm brieter Perforation/Kammer-Anordnung. Koln: DFVLR, 1986.
Find full textQin, Ning, Jacques Periaux, and Gabriel Bugeda, eds. Advances in Effective Flow Separation Control for Aircraft Drag Reduction. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-29688-9.
Full textduP, Donaldson Coleman, Donaldson Coleman duP, Aeronautical Research Associates of Princeton, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center, eds. A fundamental study of drag and an assessment of conventional drag-due-to-lift reduction devices. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textLuc, Huyse, Padula Sharon, and Langley Research Center, eds. Robust airfoil optimization to achieve consistent drag reduction over a mach range. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.
Find full textLuc, Huyse, Padula Sharon, and Langley Research Center, eds. Robust airfoil optimization to achieve consistent drag reduction over a mach range. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.
Find full textUnited States. National Aeronautics and Space Administration., ed. Computation of H2/air reacting flowfields in drag-reduction external combustion. [Washington, DC: National Aeronautics and Space Administration, 1992.
Find full textLi, Wu. Robust airfoil optimization to achieve consistent drag reduction over Mach range. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2001.
Find full textM, Gregory Irene, and Langley Research Center, eds. Trim drag reduction concepts for horizontal takeoff single-stage-to-orbit vehicles. Hampton, VA: National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textYu, Xiaoshen, and United States. National Aeronautics and Space Administration., eds. A preliminary investigation of drag reduction and mechanism for a blunt body of revolution with slanted base. Washington, DC: National Aeronautics and Space Administration, 1988.
Find full textM, Herrmann, and George C. Marshall Space Flight Center., eds. International Space Station: Electrodynamic tether reboost study. [Huntsville, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.
Find full textG, De Witt Kenneth, and United States. National Aeronautics and Space Administration., eds. Analysis and evaluation of an integrated laminar flow control propulsion system: Final technical report. [Washington, DC: National Aeronautics and Space Administration, 1993.
Find full textSaltzman, Edwin J. A reassessment of heavy-duty truck aerodynamic design features and priorities. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.
Find full textR, Meyer Robert, and NASA Dryden Flight Research Center., eds. A reassessment of heavy-duty truck aerodynamic design features and priorities. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.
Find full textR, Meyer Robert, and NASA Dryden Flight Research Center., eds. A reassessment of heavy-duty truck aerodynamic design features and priorities. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.
Find full textCoustols, E. Turbulence Control by Passive Means: Proceedings of the 4th European Drag Reduction Meeting. Dordrecht: Springer Netherlands, 1990.
Find full textEuropean, Drag Reduction Meeting (4th 1989 Lausanne Switzerland). Turbulence control by passive means: Proceedings of the 4th European Drag Reduction Meeting. Dordrecht: Kluwer Academic Publishers, 1990.
Find full textE, Mineck Raymond, and Langley Research Center, eds. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textAllison, Dennis O. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Virginia: National Aeronautics and Space Administration, Langly Research Center, 1996.
Find full textE, Mineck Raymond, and Langley Research Center, eds. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textCenter, Langley Research, ed. Noise exposure reduction of advanced high-lift systems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textE, Stanewsky, ed. Drag reduction by shock and boundary layer control: Results of the project EUROSHOCK II supported by the European Union, 1996-1999. Berlin: Springer, 2002.
Find full textAlbert, Gyr, and International Union of Theoretical and Applied Mechanics., eds. Structure of turbulence and drag reduction: IUTAM Symposium, Zurich, Switzerland, July 25-28, 1989. Berlin: Springer-Verlag, 1990.
Find full textGyr, Albert. Structure of Turbulence and Drag Reduction: IUTAM Symposium Zurich, Switzerland July 25-28, 1989. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990.
Find full textChithrabhanu, Koodalattupuram, Langley Research Center, Old Dominion University. Research Foundation, and Old Dominion University. School of Engineering, eds. An investigation of the feasibility of active boundary layer thickening for aircraft drag reduction. Norfolk, Va: Dept. of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University, 1986.
Find full textChanson, H. Drag reduction in self-aerated flows: Analogy with dilute polymer solutions and sediment laden flows. Brisbane: University of Queensland, Dept. of Civil Engineering, 1992.
Find full textChanson, H. Drag reduction in self-aerated flows: Analogy with dilute polymer solutions and sediment laden flows. Brisbane: Department of Civil Engineering, University of Queensland, 1992.
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