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Book Study of Three dimensional Supersonic Flow Problems by a Numerical Method Based on the Method of Characteristics Specially Adapted for Use on High Speed Electronic Digital Computers

Download or read book Study of Three dimensional Supersonic Flow Problems by a Numerical Method Based on the Method of Characteristics Specially Adapted for Use on High Speed Electronic Digital Computers written by Cheng Chih Tsung and published by . This book was released on 1961 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Study of Three dimensional Supersonic Flow Problems by a Numerical Method

Download or read book Study of Three dimensional Supersonic Flow Problems by a Numerical Method written by C. C. Tsung and published by . This book was released on 1961 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Method of Characteristics for Steady Three dimensional Supersonic Flow with Application to Inclined Bodies of Revolution

Download or read book A Method of Characteristics for Steady Three dimensional Supersonic Flow with Application to Inclined Bodies of Revolution written by John V. Rakich and published by . This book was released on 1969 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Characteristics method for determining three dimensional supersonic flow around inclined body of revolution.

Book Analysis of Three dimensional Inviscid Supersonic Flow Between a Body and an Outer Wall

Download or read book Analysis of Three dimensional Inviscid Supersonic Flow Between a Body and an Outer Wall written by W. C. Armstrong and published by . This book was released on 1976 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: The three-dimensional inviscid supersonic flow equations are solved for the flow over a body located within a duct. Numerical solutions are obtained by use of the reference plane method of characteristics technique. Results of the analysis are compared with experimental test body pressure distributions obtained with an off-design jet stretcher system. The analysis is sufficiently general so that a variety of internal flows may be predicted. A computer program listing and an example problem are presented.

Book Practical Numerical Methods of Three dimensional Supersonic Flow

Download or read book Practical Numerical Methods of Three dimensional Supersonic Flow written by Robert Sauer and published by . This book was released on 1960 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Document contains 6 short technical notes (TN 1-6) by various authors.

Book Flow Field Analysis of Aircraft Configurations Using a Numerical Solution to the Three dimensional Unified Supersonic hypersonic Small Disturbance Equations

Download or read book Flow Field Analysis of Aircraft Configurations Using a Numerical Solution to the Three dimensional Unified Supersonic hypersonic Small Disturbance Equations written by R. C. Gunness and published by . This book was released on 1972 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: The unified small disturbance equations are numerically solved using the well-known Lax-Wendroff finite difference technique. The method allows complete determination of the inviscid flow field and surface properties as long as the flow remains supersonic. Shock waves and other discontinuities are accounted for implicity in the numerical method. This technique was programed for general application to the three-dimensional case. The validity of the method is demonstrated by calculations on cones, axisymmetric bodies, lifting bodies, delta wings, and a conical wing/body combination. Part 1 contains the discussion of problem development and results of the study. Part 2 contains flow charts, subroutine descriptions, and a listing of the computer program.

Book Practical Numerical Methods of Three dimensional Supersonic Flows

Download or read book Practical Numerical Methods of Three dimensional Supersonic Flows written by R. Sauer and published by . This book was released on 1963 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two new difference methods for the numerical solution of initial value problems in quasilinear partial differential equations were developed. One of these methods is applied to problems of the propagation of non-linear pressure waves. Some other investigations now under way, concerning questions in quasilinear equations are briefly discussed. (Author).

Book Three dimensional Supersonic Flow Fields Some Numerical Results

Download or read book Three dimensional Supersonic Flow Fields Some Numerical Results written by F. Walkden and published by . This book was released on 1972 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Second order Numerical Method of Characteristics for Three dimensional Supersonic Flow

Download or read book A Second order Numerical Method of Characteristics for Three dimensional Supersonic Flow written by Victor Harvey Ransom and published by . This book was released on 1975 with total page 434 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Numerical Analysis of a Method for Calculating Three dimensional Supersonic Flow Fields

Download or read book Numerical Analysis of a Method for Calculating Three dimensional Supersonic Flow Fields written by Jerome J. Brainerd and published by . This book was released on 1967 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: The stability and error of a method of near-characteristics computer program are studied. A scheme for 'almost' second-order integration of the equations and a rapidly convergent shock calculation method are proposed. In addition, a technique to insure automatic fulfillment of the CFL condition is described. (Author).

Book An Introduction to Compressible Flows with Applications

Download or read book An Introduction to Compressible Flows with Applications written by José Pontes and published by Springer Nature. This book was released on 2019-12-02 with total page 129 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book offers a concise and practical survey of the principles governing compressible flows, along with selected applications. It starts with derivation of the time-dependent, three-dimensional equation of compressible potential flows, and a study of weak waves, including evaluation of the sound speed in gases. The following chapter addresses quasi-one-dimensional flows, the study of normal shock waves, and flow in ducts with constant cross section subjected to friction and/or heat transfer. It also investigates the effects of friction and heat transfer in ducts with variable cross section. The chapter ends by pointing to the analogy between one-dimensional compressible flows and open channel hydraulics. Further, the book discusses supersonic flows, including the study of oblique shock waves, and supersonic flows over corners and wedges. It also examines Riemann problems, numerical resolution of the wave equation, and of nonlinear hyperbolic problems, including propagation of strong waves. A subsequent chapter focuses on the small perturbation theory of subsonic, transonic and supersonic flows around slender bodies aligned or almost aligned to the uniform inflow. In particular, it explores subsonic and supersonic flows over a wavy wall. Lastly, an appendix with a short derivation of the Fluid Mechanics basic equations is included. The final chapter addresses the problem of transonic flows where both subsonic and supersonic are present. Lastly, an appendix with a short derivation of the Fluid Mechanics basic equations is included. Illustrated with several practical examples, this book is a valuable tool to understand the most fundamental mathematical principles of compressible flows. Graduate Mathematics, Physics and Engineering students as well as researchers with an interest in the aerospace sciences benefit from this work.