Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Supersonic Flow About Cones At Large Angles Of Attack
Download Supersonic Flow About Cones At Large Angles Of Attack full books in PDF, epub, and Kindle. Read online Supersonic Flow About Cones At Large Angles Of Attack ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Charts for the Analysis of Supersonic Flow Around Cones at Large Angles of Attack by : Emory Vanoy Mobley
Download or read book Charts for the Analysis of Supersonic Flow Around Cones at Large Angles of Attack written by Emory Vanoy Mobley and published by . This book was released on 1959 with total page 262 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Flow about Cones at Large Angles of Attack by : Clive Allen John Fletcher
Download or read book Supersonic Flow about Cones at Large Angles of Attack written by Clive Allen John Fletcher and published by . This book was released on 1974 with total page 294 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical method is presented which is applicable to the supersonic inviscid flow about cones inclined at such angles of attack that a substantial region of supersonic crossflow exists (M sub cr 1). The method is based partly on the method of Gilinskii, Telenin and Tinyakov and partly on the method of characteristics. The method produces results that compare favorably with experimental data and with the results of other numerical methods. The numerical method has produced results in the range: free stream Mach number =3 to 16; incidence, alpha = 10 to 50 deg, nose cone angles, theta sub b = 5 to 30 deg. These results demonstrate similar trends with free stream Mach number, alpha and theta sub b as obtained for subsonic crossflow Mach numbers (m sub cr
Book Synopsis Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack by : Joseph L. Sims
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:
Book Synopsis Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack by : Joseph L. Sims
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 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computation of the Inviscid Supersonic Flow about Cones at Large Angles of Attack by a Floating Discontinuity Approach by : James Edward Daywitt
Download or read book Computation of the Inviscid Supersonic Flow about Cones at Large Angles of Attack by a Floating Discontinuity Approach written by James Edward Daywitt and published by . This book was released on 1977 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Flow Around Right Circular Cones, Tables for Zero Angle of Attack by : Joseph L. Sims
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:
Book Synopsis Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack by : Joseph L. Sims
Download or read book Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1973 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of the calculation of supersonic flow of helium about right circular cones at zero angle of attack are presented in tabular form. The calculations were performed using the Taylor-Maccoll theory. Numerical integrations were performed using a Runge-Kutta method for second-order differential equations. Results were obtained for cone angles from 2.5 to 30 degrees in regular increments of 2.5 degrees. In all calculations the desired free-stream Mach number was obtained to five or more significant figures.
Book Synopsis Tables for Supersonic Flow Around Right Ciruclar Cones at Zero Angle of Attack by : Joseph L. Sims
Download or read book Tables for Supersonic Flow Around Right Ciruclar Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1964 with total page 428 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Flow Around Cones at Large Yaw by : G. B. W. YOUNG
Download or read book Supersonic Flow Around Cones at Large Yaw written by G. B. W. YOUNG and published by . This book was released on 1951 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: Equations were developed for the flow properties in the region bounded by a supersonic cone body at large angle of attack and its attached shock wave, for use with the tabulations of Kopal. A comparison of the theoretical results is made with the experimental data of Cronvich. A slight discrepancy which increases with increasing Mach number was found in the value of K sub DYH, the yawing head drag as tabulated by Kopal. (Author).
Book Synopsis Laminar Boundary Layer on Cone in Supersonic Flow at Large Angle of Attack by : Franklin K. Moore
Download or read book Laminar Boundary Layer on Cone in Supersonic Flow at Large Angle of Attack written by Franklin K. Moore and published by . This book was released on 1953 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt: The laminar-boundary-layer flow about a cone at large angles of attack to a supersonic stream has been analyzed in the plane of symmetry. At the bottom of the cone, velocity profiles were obtained showing the expected tendency of the boundary layer to become thinner on the under side of the cone as the angle of attack is increased. At the top of the cone, the analysis failed to yield unique solutions, except for small angles of attack. Beyond a certain critical angle of attack, boundary-layer flow does not exist in the plane of symmetry, thus indicating separation.
Book Synopsis An Experimental Investigation of Supersonic Flow Past Circular Cones at High Angles of Attack by : Abdollah Modavi
Download or read book An Experimental Investigation of Supersonic Flow Past Circular Cones at High Angles of Attack written by Abdollah Modavi and published by . This book was released on 1978 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamics of Large-angle Cones by : James F. Campbell
Download or read book Supersonic Aerodynamics of Large-angle Cones written by James F. Campbell and published by . This book was released on 1968 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Massachusetts Institute of Technology. Department of Electrical Engineering. Center of Analysis Publisher : ISBN 13 : Total Pages :154 pages Book Rating :4.:/5 (89 download)
Book Synopsis Tables of Supersonic Flow Around Cones of Large Yaw by : Massachusetts Institute of Technology. Department of Electrical Engineering. Center of Analysis
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:
Book Synopsis Laminar Boundary Layer on a Circular Cone in Supersonic Flow at a Small Angle of Attack by : Franklin K. Moore
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.
Book Synopsis Supersonic Lifting Capabilities of Large-angle Cones by : James F. Campbell
Download or read book Supersonic Lifting Capabilities of Large-angle Cones written by James F. Campbell and published by . This book was released on 1969 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics of large-angle cones in supersonic lifting capabilities.
Book Synopsis Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 by : Jerome D. Julius
Download or read book Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 written by Jerome D. Julius and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-angle Cones with and Without Cylindrical Afterbodies by : James Franklin Campbell
Download or read book Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-angle Cones with and Without Cylindrical Afterbodies written by James Franklin Campbell and published by . This book was released on 1969 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and without cylindrical afterbodies.