Download or read book Supersonic Lift Solutions Obtained by Extending the Simple Linearized Conical Flow Theory written by T. F. Coleman and published by . This book was released on 1947 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of the linearized conical supersonic flow theory for flat plate wings are extended to the treatment of certain planforms which cannot be solved by the simple methods of superposition previously described. The method described in the report is applicable to wings with subsonic trailing edges (within certain limitations) and to regions in which the flow is affected by more than one disturbance. Solutions are obtained by superposing conical flow fields resulting from elementary wings with certain special properties, to the basic wings required; this superposition is accomplished by integrating the contribution of an infinite number of such elementary wings, plus the contributions from the basic wings obtained in the usual manner. The elementary wings used are chosen in such a way that the boundary conditions of the wing to be solved are satisfied by the integrated solution. The method is applied to obtain expressions for the pressure distributions on a low aspect ratio rectangular wing, a triangular wing with cut-off wing tips, and a diamond wing. (Author).
Download or read book linearized theory of steady high speed flow written by and published by CUP Archive. This book was released on with total page 268 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Linearized Theory of Steady High Speed Flow written by G. N. Ward and published by Cambridge University Press. This book was released on 2016-02-25 with total page 261 pages. Available in PDF, EPUB and Kindle. Book excerpt: Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Download or read book High Speed Wing Theory written by Doris Cohen and published by Princeton University Press. This book was released on 2015-12-08 with total page 251 pages. Available in PDF, EPUB and Kindle. Book excerpt: Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Download or read book U S Government Research and Development Reports written by and published by . This book was released on 1965 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 878 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Lifting Surfaces in Supersonic Flow Linearized three dimensional theory by W H Pell written by Simon Ostrach and published by . This book was released on 1949 with total page 646 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Analysis of the Effects of Boundary layer Control on the Power off Landing Performance Characteristics of a Liaison Type of Airplane written by Elmer A. Horton and published by . This book was released on 1950 with total page 678 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made to determine the effects of boundary-layer control on the landing performance characteristics of a liaison type of airplane having a payload of 1500 pounds and a flight duration of 5 hours. The aspect ratio was varied from 5 to 15, the wing span from 30 to 100 feet, and the brake horsepower from 300 to 1200. The use of boundary-layer control caused reduction in total landing distance (25 to 40 percent), ground-run distance, gliding speed, and stalling speed whereas sinking speed was increased only slightly.
Download or read book Aerodynamic Components of Aircraft at High Speeds written by Allen F. Donovan and published by Princeton University Press. This book was released on 2015-12-08 with total page 863 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Correlation of Physical Properties with Molecular Structure for Some Dicyclic Hydrocarbons Having High Thermal energy Release Per Unit Volume written by Alexander Mendelson and published by . This book was released on 1950 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1950 with total page 996 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamics of Supersonic Lifting Bodies written by Martin C. Jischke and published by . This book was released on 1981 with total page 414 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a combined theoretical and experimental program of research in the aerodynamics of supersonic lifting bodies. Analytical perturbation techniques are used to study the supersonic flow past slightly elliptical cones, cones whose cross-sections deviate slightly but arbitrarily from that of a right circular cone, cones of small longitudinal curvature, and right circular cones undergoing small harmonic pitching and/or plunging motions. These studies all involve perturbations of the well-known solution for supersonic flow past a right circular cone. Closed-form analytical results are achieved through the use of an approximation that accurately predicts results over the entire range of the hypersonic similarity parameter. These results give hypersonic limiting solutions that agree well with other independent analyses and, at the same time, agree exactly with linearized theory in the linear theory limit. Comparisons with experiment, where possible, also show good agreement.
Download or read book Annual Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Download or read book Linearized Supersonic Flow written by Wallace Dean Hayes and published by . This book was released on 1947 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Application of the Linearized Theory of Supersonic Flow to the Estimation of Control Surface Characteristics written by and published by . This book was released on 1948 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: Known conical-flow solutions of the linearized equation for the velocity potential in supersonic flow are applied to the calculation of the characteristics of control surfaces Complete solutions for the pressure distributions are obtained for control surfaces with hinge lines swept ahead of or behind the Mach line when the control-surface trailing edge is swept ahead of the Mach line. Useful approximate solutions of good accuracy are obtained when the trailing edge is swept behind the Mach line. Applications of the theory to the estimation of the hinge-moment and effectiveness characteristics of elevators and ailerons are presented.
