Download or read book Study of Subsonic Transonic and Supersonic Flow Over a Cone written by Robert C. Lock and published by . This book was released on 1973 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Numerical Methods for Predicting Subsonic Transonic and Supersonic Flow written by Thomas Darwin Taylor and published by . This book was released on 1974 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The methods available for numerical computation of subsonic, transonic and supersonic flows are discussed and comments are included on the characteristics of the popular methods. Both inviscid and viscous computation methods are addressed. A brief account of the basic approaches for developing methods initiates the discussion. Also included is a general summary of the state of the art of computational methods along with suggested approaches for solving problems in each area. The report is included with recommendations for future study and development. (Author).
Download or read book Some Fluid Mechanical Problems Related to Subsonic and Supersonic Aircraft written by United States. National Aeronautics and Space Administration. Ad Hoc Committee on Subsonic and Supersonic Aeronautics and published by . This book was released on 1968 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Research on Transonic and Supersonic Flow of a Real Fluid at Abrupt Increases in Cross Section with Special Consideration of Base Drag Problems written by Helmut Hans Korst and published by . This book was released on 1964 with total page 330 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Computation of Supersonic Flow over Flying Configurations written by Adriana Nastase and published by Elsevier. This book was released on 2010-07-07 with total page 425 pages. Available in PDF, EPUB and Kindle. Book excerpt: Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. Computational work and experimental results show the real-world application of computational results Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations Includes a fully optimized and integrated design for a proposed supersonic transport aircraft
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 Contributions to the Development of Gasdynamics written by Klaus Oswatitsch and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt: Ever since airplane speeds started to approach the speed of sound, the study of compressible flow problems attracted much talent and support in the major indus trialized countries. Today, gas dynamics is a mature branch of science whose many aspects and applications are much too numerous to be mastered by a single person or to be described in a few volumes. This book commemorates the 70th birthday of a great pioneer and teacher of gas dynamics, Dr. Klaus Oswatitsch, Professor of Fluid Mechanics at the Technical University of Vienna and former Director of the Institute for Theoretical Gas Dyna mics, Deutsche Forschungs-und Versuchsanstalt fUr Luft-und Raumfahrt. Several reasons motivated us to prepare an English translation of Oswatitsch's selected sci entific papers. First, we hope that a book containing his major papers will be wel come as a valuable reference text in gas dynamics. Oswatitsch's work is frequently used in the literature in one form or another, but it is usually quite time-consuming for the English speaking reader to consult the original texts. As a result, reference to and understanding of his papers is often incomplete. For example, Oswatitsch's formulation of the equivalence rule hardly ever is quoted in recent textbooks, al though it preceded declassification of Whitcomb's results by several years. Further more, his papers contain much information, which has not yet been fully appreciated in the Anglo-American literature.
Download or read book Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack written by Joseph L. Sims and published by . This book was released on 1964 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control written by Benjamin Milwitzky and published by . This book was released on 1955 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Calculation of Linearized Supersonic Flow Over Slender Cones of Arbitrary Cross Section written by Vincent Robert Mascitti and published by . This book was released on 1972 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Supersonic linearized conical-flow theory is used to determine the flow over slender pointed cones having horizontal and vertical planes of symmetry. The geometry of the cone cross sections and surface velocities are expanded in Fourier series. The symmetry condition permits the uncoupling of lifting and nonlifting solutions. The present method reduces to Ward's theory for flow over a cone of elliptic cross section. Results are also presented for other shapes. Results by this method diverge for cross-sectional shapes where the maximum thickness is large compared with the minimum thickness. However, even for these slender-body shapes, lower order solutions are good approximations to the complete solution.
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 An Experimental Study of Supersonic Flows Over an Elliptic Cone written by and published by . This book was released on 1999 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An elliptic cone similar to the one used by other investigators, a 4:1 aspect ratio elliptic cone with the cone angle on the major axis of 17.5 deg and 4.5 deg along the minor axis, in a Mach 2.8 tunnel was used in the present work. The Reynolds number used in this work was much higher than that used in other experimental work. The purpose is to examine the transition process as well as the turbulent structure of a three-dimensional boundary layer after transition. The primary focus of this study is on the structure of the turbulence, which was explored using advanced optical diagnostics. Both surface flow visualizations and Filtered Rayleigh Scattering (FRS) based flow visualizations were used in this study. The results showed that the boundary layer developing along the major centerline, the flattest region on the cone surface, underwent transition to turbulence approximately 35 mm downstream of the cone tip. Surface cross flow was observed primarily near the minor centerline of the cone, the area with the largest curvature. No cross flow was observed around the major centerline after 10 mm downstream of the cone tip.
Download or read book A Description of Numerical Methods and Computer Programs for Two dimensional and Axisymmetric Supersonic Flow Over Blunt nosed and Flared Bodies written by Mamoru Inouye and published by . This book was released on 1965 with total page 42 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 1955 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
