Download or read book An Example for the Practical Calculation of Supersonic Flow Fields Past Oscillating Bodies of Revolution by a Method Due to Sauer written by Johann Muench and published by . This book was released on 1958 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book AFOSR written by United States. Air Force. Office of Scientific Research and published by . This book was released on 1957 with total page 1136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Techniques for Measurement of Dynamic Stability Derivatives in Ground Test Facilities written by Clarence John Schueler and published by . This book was released on 1967 with total page 242 pages. Available in PDF, EPUB and Kindle. Book excerpt: Some of the techniques in current use for measuring dynamic stability derivatives in wind tunnels are described, with emphasis given to the important features of balance system design, data reduction methods, instrumentation and typical balance systems. The use of gas bearings for dynamic stability and roll damping balances is treated and a three-degree-of-freedom balance system employing a spherical gas bearing is described. (Author).
Download or read book An Improved Method for Calculating Supersonic Pressure Fields about Bodies of Revolution written by Robert J. Mack and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Development of near-field method for determining supersonic flow properties about bodies of revolution.
Download or read book Calculation of Supersonic Flow Past Slowly Oscillating Bodies of Revolution by Use of Electronic Computers written by Johann Muench and published by . This book was released on 195? with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Air Force Scientific Research Bibliography written by Library of Congress. Science and Technology Division and published by . This book was released on 1961 with total page 1130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Air Force Scientific Research Bibliography 1957 58 written by Library of Congress. Science and Technology Division and published by . This book was released on 1964 with total page 1130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Recent Advances in the Theory of Supersonic Flow written by Robert Sauer and published by . This book was released on 1951 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains a series of lectures on supersonic and hypersonic flow delivered at the Naval Ordnance Laboratory during the summer of 1950. The subject matter covers a number of advanced topics in the field of aeroballistics, based on research carried out recently by the author. The results are applicable to the solution of aerodynamic problems in the design of supersonic and hypersonic missiles. An exposition is given of methods to calculate flow about slowly oscillating bodies as well as past yawing bodies of revolution. The report is written in four sections: (1) partial differential equations with straight-line characteristics; (2) slowly oscillating bodies in linearized supersonic flow; (3) supersonic and hypersonic flow past yawing, bodies of revolution; (4) the method of characteristics in three-dimensional supersonic flow.
Download or read book Practical Calculation of Second order Supersonic Flow Past Nonlifting Bodies of Revolution written by Milton Van Dyke and published by . This book was released on 1952 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation of second-order supersonic flow past bodies of revolution at zero angle of attack is described in detail, and reduced to routine computation. Use of an approximate tangency condition is shown to increase the accuracy for bodies with corners. Tables of basic functions and standard computing forms are presented. The procedure is summarized so that one can apply it without necessarily understanding the details of the theory. A sample calcuation is given, and several examples are compared with solutions calculated by the method of characteristics.
Download or read book Calculation of Supersonic Flow Past Bodies Supporting Shock Waves Shaped Like Elliptic Cones written by Benjamin R. Briggs and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aero space Engineering written by and published by . This book was released on 1959 with total page 1386 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Study of Methods which Predict Supersonic Flow Fields from Body Geometry Distance and Mach Number written by Robert J. Mack and published by . This book was released on 1973 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Time dependent Method for Calculating Supersonic Angle of attack Flow about Axisymmetric Blunt Bodies with Sharp Shoulders and Smooth Nonaxisymmetric Blunt Bodies written by Richard W. Barnwell and published by . This book was released on 1971 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: A time-dependent numerical method for calculating supersonic flow about blunt bodies at large angles of attack is presented. The axisymmetric bodies with sharp shoulders which are treated are constructed with a generator composed of segments of constant curvature. The nonaxisymmetric bodies have continuous slope and curvature. All flow fields are inviscid and adiabatic and have one plane of symmetry. A modification to the method of characteristics is introduced for use at the shock wave. A two-step finite-difference method of second-order accuracy is used at the body surface and in the region between the shock and body. A new finite-difference technique is introduced for use at sharp sonic shoulders. Comparisons of the results of the present method with experiment and the results of other methods are made for the flow of equilibrium air past the Apollo command module at the trim angle of attack and for perfect gas flow past a spherical cap and a spherically blunted cone at angle of attack. Both the cap and the blunted cone are terminated with sharp shoulders. Results are presented also for perfect gas flow past a prolate spheroid with its major axis normal to the flow.
Download or read book Velocity Potential and Forces on Oscillating Slender Bodies of Revolution in Supersonic Flow Expanded to the Fifth Power of the Frequency written by Donald L. Lansing and published by . This book was released on 1962 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1967 with total page 742 pages. Available in PDF, EPUB and Kindle. Book excerpt:
