Download or read book Analysis of Supersonic Conical Flows written by C. W. Chiang and published by . This book was released on 1970 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Analysis of Supersonic Flow Phenomena in Conical Nozzles by a Method of Characteristics written by Linwood B. Callis and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Study of Supersonic Conical Flow written by Masahiro Kurosaki and published by . This book was released on 1973 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Flow Around Right Circular Cones Tables for Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1960 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Conical Flow written by Stephen H. Maslen and published by . This book was released on 1952 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical method is described for the solution of the nonlinear equations for supersonic conical flow. The procedure is a combination of the method of characteristics and the relaxation process. A method for calculating the position of the shock is inherent in the analysis. The method presented is applicable to any conical flow and a solution for the flow about a triangular wing with supersonic leading edges is included as an illustration.
Download or read book Analysis of the Linearized Supersonic Flow about Pointed Bodies of Revolution by the Method of Characteristics written by Alan D. Sherer and published by . This book was released on 1966 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Analysis of the Three dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow written by John C. Adams and published by . This book was released on 1972 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.
Download or read book General Theory of Conical Flows and Its Application to Supersonic Aerodynamics written by Paul Germain and published by . This book was released on 1955 with total page 354 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report deals with a method of studying the equation of cylindrical waves particularly indicated for the solution of certain aerodynamic problems. The method reduces problems of a hyperbolic equation to problems of harmonic functions. The study has been applied toward setting up the fundamental principles, to developing their investigation up to calculation of the pressures on the visualized obstacles, and to showing how the initial field of "conical flows" was considerably enlarged by a procedure of integral superposition.
Download or read book Generalized Conical flow Fields in Supersonic Wing Theory written by Harvard Lomax and published by . This book was released on 1951 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: Linearized, compressible-flow analysis is applied to the study of quasi-conical supersonic wing theory. Single-integral equations are derived which relate either the loading to the shape of a lifting surface or the thickness of a symmetrical wing to the pressure distribution for triangular wings to the pressure distribution for triangular wings with subsonic leading edges. The forms of these equations and their inversions are simplified thorugh the introduction of the finite part and the generalized part of an integral. Applications to the theory, in the lifting case, include previously known results. In the non-lifing case, it is shown that for a specified pressure distribution the theory does not always predict a unique thickness distribution. This is demonstrated for a triangular plan form having a constant pressure gradient in the stream direction.
Download or read book A Study of Flow about Objects Traveling at High Supersonic Speeds written by Alfred John Eggers (Jr.) and published by . This book was released on 1956 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Laminar Boundary Layer on a Circular Cone in Supersonic Flow at a Small Angle of Attack written by Franklin K. Moore and published by . This book was released on 1951 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: The laminar boundary layer on a circular cone at angle of attack to a supersonic stream is discussed. A perturbation analysis was made to show the influence of a small angle of attack on such boundary layer quantities as skin friction, boundary-layer thickness, viscous lift, drag, and pitching moment.
Download or read book Tables of Supersonic Flow Around Cones of Large Yaw written by Massachusetts Institute of Technology. Department of Electrical Engineering. Center of Analysis and published by . This book was released on 1949 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Flow about Right Circular Cones at Zero Yaw in Air at Thermodynamic Equilibrium Part Ii Tables of Data written by Henry E Hudgins (Jr) and published by . This book was released on 1964 with total page 825 pages. Available in PDF, EPUB and Kindle. Book excerpt: Part I (AD-468 284) of this report is an analysis of the inviscid flow fields for air in chemical equilibrium about right circular cones at zero yaw. Parts II and III present, in tabular form, the results of the calculation of real gas supersonic flow fields about right circular cones at zero angle of yaw upon which the correlation analysis in Part I is based. The calculations were performed by a numerical integration of the conical flow equations written in terms of a single geometric parameter, the ray angle eta; thus, the results are independent of body size. Flow properties are given along rays which are defined by 10 equal angular increments between the shock and cone surface. Numerical calculations were performed utilizing the Picatinny Arsenal IBM 709/90/94 Conical Flow Field Program. Results are obtained for cone semi-angles from 2.5 degrees to 50 degrees, altitudes from 0 to 200,000 ft, and Mach numbers from 3 to 40, excluding those which result in a detached shock or are well within the ideal gas regime. (Author).
Download or read book Infinitesimal Conical Supersonic Flow written by Adolf Busemann and published by . This book was released on 1947 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The calculation of infinitesimal conical supersonic flow has been applied first to the simplest examples that have also been calculated in another way. Except for the discovery of a miscalculation in an older report, there was found the expected conformity. The new method of calculation is limited more definitely to the conical case.
Download or read book Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1964 with total page 462 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 Use of a Characteristic Surfaces for Unsymmetrical Supersonic Flow Problems written by Wolfgang E. Moeckel and published by . This book was released on 1949 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: Application of the method of characteristics to the linearized three-dimensional equation results in a relatively simple system of difference equations that can be used to compute the supersonic flow past boundaries for which no other linearized solutions are available.
