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Calculation Of The Force Coefficient For Delta Wings In Hypersonic Flow
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Book Synopsis Calculation of the Force Coefficient for Delta Wings in Hypersonic Flow by : Arnold Polak
Download or read book Calculation of the Force Coefficient for Delta Wings in Hypersonic Flow written by Arnold Polak and published by . This book was released on 1965 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of the Newtonian theory as applied to a delta wing at moderate angles of attack in hypersonic stream are used to calculate the pressure coefficient by the inverse method in a closed form. (Author).
Book Synopsis Wing Theory in Supersonic Flow by : Elie Carafoli
Download or read book Wing Theory in Supersonic Flow written by Elie Carafoli and published by Elsevier. This book was released on 2013-10-22 with total page 611 pages. Available in PDF, EPUB and Kindle. Book excerpt: Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the characteristics of drag, lift, and moments for various shapes of the trailing edge line. This book discusses as well the wings of ordinary shapes, delta wings, yawed wings, polygonal wings, trapezoid wings, and arrow-head or swept-back wings. The final chapter deals with a delta wing with a central fusiform body. This book is a valuable resource for teachers, students, and specialists engaged in modern aerodynamics.
Book Synopsis An Analysis of the Delta-wing Hypersonic Stability and Control Behavior at Angles of Attack Between 30° and 90° by : David E. Fetterman
Download or read book An Analysis of the Delta-wing Hypersonic Stability and Control Behavior at Angles of Attack Between 30° and 90° written by David E. Fetterman and published by . This book was released on 1963 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method for Calculating the Aerodynamic Forces Due to Arbitrary, Time Dependent Downwash for a Class of Thin, Flexible Wings at Supersonic Speeds by : Robert W. Warner
Download or read book A Method for Calculating the Aerodynamic Forces Due to Arbitrary, Time Dependent Downwash for a Class of Thin, Flexible Wings at Supersonic Speeds written by Robert W. Warner and published by . This book was released on 1960 with total page 72 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 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method for Calculating the Generalized Aerodynamic Forces on Rectangular Wings Deforming Symmetrically in Supersonic Flight with Indicial Or Sinusoidal Time Dependence by :
Download or read book A Method for Calculating the Generalized Aerodynamic Forces on Rectangular Wings Deforming Symmetrically in Supersonic Flight with Indicial Or Sinusoidal Time Dependence written by and published by . This book was released on 1962 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fundamentals of Modern Unsteady Aerodynamics by : Ülgen Gülçat
Download or read book Fundamentals of Modern Unsteady Aerodynamics written by Ülgen Gülçat and published by Springer Science & Business Media. This book was released on 2010-09-30 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this textbook, the author introduces the concept of unsteady aerodynamics and its underlying principles. He provides the readers with a full review of fundamental physics of the free and the forced unsteadines, the terminology and basic equations of aerodynamics ranging from incompressible flow to hypersonics. The book also covers the modern topics concerning the developments made during the last years, especially in relation to wing flappings for propulsion. The book is written for graduate and senior year undergraduate students in Aerodynamics, and it serves as a reference for experienced researchers. Each chapter includes ample examples, questions, problems and relevant references.
Book Synopsis Research on Hypersonic Flow of Blunt Delta Wings. Part I. Theoretical and Experimental Study of a 70-degree Blunt Delta Wing for Low Angles of Attack at Supersonic and Hypersonic Speeds by : Bernard Mazelsky
Download or read book Research on Hypersonic Flow of Blunt Delta Wings. Part I. Theoretical and Experimental Study of a 70-degree Blunt Delta Wing for Low Angles of Attack at Supersonic and Hypersonic Speeds written by Bernard Mazelsky and published by . This book was released on 1967 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: The object of the present analysis is to investigate the high-speed aerodynamic properties of a blunt delta wing at low angles of attack where the maximum lift to drag ratio occurs. Oguchi's solution of hypersonic flow over a blunt leading edge flat plate at zero incidence is extended to three dimensional delta wings at angle of attack. The shock wave shapes and pressure distributions were obtained by employing the oblique shock relations at the windward sides of the Prandtl-Meyer equations at the leeward side of the wing. The total lift and drag of the wing due to pressure and skin friction were computed by numerical integration using the IBM 7094 computer. The present calculated aerodynamic forces generally agree with the experimental data at the high supersonic Mach numbers (M approx.> or = 4) and lower thickness ratio of the wing which is a 70-degree swept slab sided delta wing with a cylindrical leading edge. (Author).
Book Synopsis A Second Order Slender Wing Theory for Wings with Leading Edge Separation in Supersonic Flow by : Joseph P. Nenni
Download or read book A Second Order Slender Wing Theory for Wings with Leading Edge Separation in Supersonic Flow written by Joseph P. Nenni and published by . This book was released on 1971 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Unsteady Aerodynamics and Control of Delta Wings with Tangential Leading Edge Blowing by : Stanford University. Department of Aeronautics and Astronautics
Download or read book Prediction of Unsteady Aerodynamics and Control of Delta Wings with Tangential Leading Edge Blowing written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on 1989 with total page 396 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method for Predicting the Normal-force Characteristics of Delta Wings at Angles of Attack from 0 Deg to 90 Deg by :
Download or read book A Method for Predicting the Normal-force Characteristics of Delta Wings at Angles of Attack from 0 Deg to 90 Deg written by and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computation of a Delta-wing Roll-and-hold Maneuver by : Raymond E. Gordnier
Download or read book Computation of a Delta-wing Roll-and-hold Maneuver written by Raymond E. Gordnier and published by . This book was released on 1993 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents computations of the flowfield around an 80 degree sweep delta wing undergoing a constant roll-rate maneuver from 0 to 45 degrees. The governing equations for the problem are the unsteady, three- dimensional Navier-Stokes equations. The equations are solved using the implicit, approximately-factored algorithm of Beam-Warming. Fixed roll angle results are also presented and compared with experimental measurements to demonstrate the ability of the numerical technique to accurately capture the flowfield around a rolled delta wing. The dynamic behaviors of the vortex position and strength, as well as their corresponding effect on surface pressure, lift and roll moment, are described. A simple, quasi-static explanation of these vortex behaviors based on effective angle-of-attack and sideslip angle is proposed ... Delta wing roll, Vortex dynamics, Vortical flow, Unsteady maneuver.
Book Synopsis Supersonic Aerodynamics of Delta Wings by : Richard M. Wood
Download or read book Supersonic Aerodynamics of Delta Wings written by Richard M. Wood and published by . This book was released on 1988 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory by : E. L. Clark
Download or read book Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory written by E. L. Clark and published by . This book was released on 1964 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: The pressure distribution predicted by the modified Newtonian theory is used to develop equations for the aerodynamic forces, moments, and stability derivatives for components of hypersonic lifting configurations. In conjunction with the equations, a set of charts is presented to enable simple determination of the aerodynamic characteristics of swept cylinders, swept wedges, spherical segments, and cone frustums at zero sideslip and angles of attack from 0 to 180 degrees. This method allows evaluation of most delta wing-body combinations without the need for numerical or graphical integration. As an example of the procedure, the theoretical characteristics of a blunt 75-degree swept delta wing are calculated and compared with experimental results.
Book Synopsis Calculation of the Heat Transfer on the Windward Side of a Delta Wing in Hypersonic Flow by : Stephen Sacks
Download or read book Calculation of the Heat Transfer on the Windward Side of a Delta Wing in Hypersonic Flow written by Stephen Sacks and published by . This book was released on 1972 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computer program has been written to calculate the heat transfer on the windward side of a delta wing in hypersonic flow. The program utilizes the small crossflow theory of Vaglio-Laurin. Heat transfer values are calculated for both the laminar and turbulent boundary layer cases, and results are compared with experimental data on delta wings available in the literature. (Author).
Book Synopsis Flow Fields Over Sharp Edged Delta Wings with Attached Shocks by : S. A. Powers
Download or read book Flow Fields Over Sharp Edged Delta Wings with Attached Shocks written by S. A. Powers and published by . This book was released on 1971 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 760 pages. Available in PDF, EPUB and Kindle. Book excerpt:
