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An Experimental Investigation Of An Airfoil Optimized For High Lift
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Book Synopsis An Experimental Investigation of an Airfoil Optimized for High Lift by : Richard E. Walters
Download or read book An Experimental Investigation of an Airfoil Optimized for High Lift written by Richard E. Walters and published by . This book was released on 1974 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was performed on an airfoil optimized for maximum lift. The airfoil shape was designed from an optimum pressure distribution using a calculus of variation technique. The purpose of the investigation was to evaluate the validity of the method of design of the airfoil, and to determine what type of differences existed, if any, in the theoretical and experimental results. The airfoil was tested at a Reynolds number approximating the design Reynolds number of 1,000,000. The airfoil angle of attack was varied in 2 deg increments from 0 deg to 12 deg. At each angle of attack, three blowing rates were used for slots installed on the model end plates. Data recorded for each test run consisted of the airfoil static pressure distribution, static and total pressures from a wake traverse, atmospheric pressure and temperature, and the tunnel temperature. Normal and chordwise force coefficients were obtained from the static pressure data. Using the true angles of attack from potential flow theory, lift and pressure drag coefficients were found. Total drag coefficients were found from the wake traverse data. Increased blowing caused the experimental pressure coefficient distributions at higher angles of attack to come into close agreement with the theoretical pressure coefficient distribution, and resulted in increased lift and decreased drag. True two-dimensional flow was not maintained at the higher angles of attack, due at least in part to the test installation. (Author).
Book Synopsis An Experimental Investigation of High Rate/high Lift Aerodynamics of an Unsteady Airfoil by : Kim Fong Yeow
Download or read book An Experimental Investigation of High Rate/high Lift Aerodynamics of an Unsteady Airfoil written by Kim Fong Yeow and published by . This book was released on 1989 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of High Lift/high Rate Aerodynamics of an Unsteady Airfoil by : G. M. Graham
Download or read book An Experimental Investigation of High Lift/high Rate Aerodynamics of an Unsteady Airfoil written by G. M. Graham and published by . This book was released on 1989 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Summary of Low Speed Airfoil Data by : Michael S. Selig
Download or read book Summary of Low Speed Airfoil Data written by Michael S. Selig and published by Soartech. This book was released on 1995 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis R & D Abstracts by : Technology Reports Centre (Great Britain)
Download or read book R & D Abstracts written by Technology Reports Centre (Great Britain) and published by . This book was released on 1976 with total page 536 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of a High-lift Low-drag Aerofoil by : F. H. Kelling
Download or read book Experimental Investigation of a High-lift Low-drag Aerofoil written by F. H. Kelling and published by . This book was released on 1968 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computational Fluid Flow and Heat Transfer by : Mukesh Kumar Awasthi
Download or read book Computational Fluid Flow and Heat Transfer written by Mukesh Kumar Awasthi and published by CRC Press. This book was released on 2024-04-25 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt: The text provides insight into the different mathematical tools and techniques that can be applied to the analysis and numerical computations of flow models. It further discusses important topics such as the heat transfer effect on boundary layer flow, modeling of flows through porous media, anisotropic polytrophic gas model, and thermal instability in viscoelastic fluids. This book: Discusses modeling of Rayleigh-Taylor instability in nanofluid layer and thermal instability in viscoelastic fluids Covers open FOAM simulation of free surface problems, and anisotropic polytrophic gas model Highlights the Sensitivity Analysis in Aerospace Engineering, MHD Flow of a Micropolar Hybrid Nanofluid, and IoT-Enabled Monitoring for Natural Convection Presents thermal behavior of nanofluid in complex geometries and heat transfer effect on Boundary layer flow Explains natural convection heat transfer in non-Newtonian fluids and homotropy series solution of the boundary layer flow Illustrates modeling of flows through porous media and investigates Shock-driven Richtmyer-Meshkov instability It is primarily written for senior undergraduate, graduate students, and academic researchers in the fields of Applied Sciences, Mechanical Engineering, Manufacturing Engineering, Production Engineering, Industrial engineering, Automotive engineering, and Aerospace engineering.
Book Synopsis Experimental and Computational Investigation of Lift-enhancing Tabs on a Multi-element Airfoil by : Dale L. Ashby
Download or read book Experimental and Computational Investigation of Lift-enhancing Tabs on a Multi-element Airfoil written by Dale L. Ashby and published by . This book was released on 1996 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Scientific and Technical Publications by :
Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 27th AIAA Fluid Dynamics Conference by :
Download or read book 27th AIAA Fluid Dynamics Conference written by and published by . This book was released on 1996 with total page 262 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Principles of Helicopter Aerodynamics by : J. Gordon Leishman
Download or read book Principles of Helicopter Aerodynamics written by J. Gordon Leishman and published by Cambridge University Press. This book was released on 2002-12-23 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt: Helicopters are highly capable and useful rotating-wing aircraft with roles that encompass a variety of civilian and military applications. Their usefulness lies in their unique ability to take off and land vertically, to hover stationary relative to the ground, and to fly forward, backward, or sideways. These unique flying qualities, however, come at a high cost including complex aerodynamic problems, significant vibrations, high levels of noise, and relatively large power requirements compared to fixed-wing aircraft. This book, written by an internationally recognized expert, provides a thorough, modern treatment of the aerodynamic principles of helicopters and other rotating-wing vertical lift aircraft. Every chapter is extensively illustrated and concludes with a bibliography and homework problems. Advanced undergraduate and graduate students, practising engineers, and researchers will welcome this thorough and up-to-date text on rotating-wing aerodynamics.
Book Synopsis Low-speed Experimental Investigation of a Thin, Faired, Double-wedge Airfoil Section with Nose and Trailing-edge Flaps by : Leonard M. Rose
Download or read book Low-speed Experimental Investigation of a Thin, Faired, Double-wedge Airfoil Section with Nose and Trailing-edge Flaps written by Leonard M. Rose and published by . This book was released on 1949 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: A faired, double-wedge airfoil section, 4.23 percent thick, was investigated with plain nose and trailing-edge flaps. The nose flap was 0.16 chord of the airfoil and the trailing-edge flap was 0.25 chord of the airfoil. Section lift, drag, and pitching-momnet data are presented for a Reynolds number of 5,800,000 which corresponded to a Mach number of 0.17.
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1975 with total page 952 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of an Airfoil Pitching at Moderate to High Rates to Large Angles of Attack by : Gary M. Graham
Download or read book An Experimental Investigation of an Airfoil Pitching at Moderate to High Rates to Large Angles of Attack written by Gary M. Graham and published by . This book was released on 1985 with total page 358 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of Aircraft written by and published by . This book was released on 2009 with total page 756 pages. Available in PDF, EPUB and Kindle. Book excerpt:
