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Author : Roberto Vaglio-Laurin
Publisher :
ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.:/5 (441 download)
Download or read book Viscous Hypersonic Flow Past a Slender Cone at Incidence written by Roberto Vaglio-Laurin and published by . This book was released on 1968 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : V. S. Nikolaev
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)
Download or read book Viscous Hypersonic Flow Past a Slender Cone written by V. S. Nikolaev and published by . This book was released on 1967 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : V. S. Nikolaev
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (689 download)
Download or read book Viscous Hypersonic Flow Past a Slender Cone written by V. S. Nikolaev and published by . This book was released on 1967 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : K. Stewartson
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Viscous Hypersonic Flow Past a Slender Cone written by K. Stewartson and published by . This book was released on 1963 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
![Download Viscous Hypersonic Flow Past Slender Cone [with List of References] PDF Online Free](https://books.google.com/books/content/images/frontcover/FfChwgEACAAJ?fife=w200-h370)
Author :
Publisher :
ISBN 13 :
Total Pages : 7 pages
Book Rating : 4.:/5 (18 download)
Download or read book Viscous Hypersonic Flow Past Slender Cone [with List of References] written by and published by . This book was released on 1967 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H. F. Waldron
Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.E/5 ( download)
Download or read book Viscous Hypersonic Flow Over Pointed Cones at Low Reynolds Numbers written by H. F. Waldron and published by . This book was released on 1966 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Kazimierz J. Orlik-Rueckemann
Publisher :
ISBN 13 :
Total Pages : 3 pages
Book Rating : 4.:/5 (72 download)
Download or read book Oscillating Slender Cone in Viscous Hypersonic Flow written by Kazimierz J. Orlik-Rueckemann and published by . This book was released on 1971 with total page 3 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unsteady pressure distributions and stability derivatives on a slender circular cone performing oscillation in pitch in viscous hypersonic flow can be determined using the method of dynamic viscous pressure interaction developed by the present author. The method takes into account the relative motion between the body surface and the boundary-layer displacement surface and can be applied to arbitrary bodies and flow conditions, provided the relevant inviscid unsteady pressure distributions and the dependence of the boundary-layer displacement on the steady flow variables are known. In the present paper, practical closed-form formulas are given for the unsteady pressure distribution and the static and dynamic pitching moment derivatives for a slender right circular cone performing low-frequency, small-amplitude oscillation in pitch around zero mean incidence and completely submerged in the weak-interaction region of laminar boundary layer. (Author).
Author : Kam-Pui Lee
Publisher :
ISBN 13 :
Total Pages : 226 pages
Book Rating : 4.:/5 (317 download)
Download or read book Viscous-shock-layer Analysis of Hypersonic Flows Over Long Slender Vehicles written by Kam-Pui Lee and published by . This book was released on 1992 with total page 226 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : M. L. Rasmussen
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Approximation of Hypersonic Flow Past a Slender Elliptic Cone written by M. L. Rasmussen and published by . This book was released on 1979 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : T.C. Lin
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (841 download)
Download or read book Viscous Flow Over a Cone at Moderate Incidence. 2. Supersonic Boundary Layer written by T.C. Lin and published by . This book was released on 1972 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John Kliewer Wall
Publisher :
ISBN 13 :
Total Pages : 202 pages
Book Rating : 4.E/5 ( download)
Download or read book Hypersonic Flow Over a Slender Cone written by John Kliewer Wall and published by . This book was released on 1957 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : David Freedman Rogers
Publisher :
ISBN 13 :
Total Pages : 200 pages
Book Rating : 4.:/5 (115 download)
Download or read book An Analytical Study of Hypersonic Viscous Flow Over an Unyawed Slender Cone at Moderately Low Densities written by David Freedman Rogers and published by . This book was released on 1967 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Lawrence Talbot
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (25 download)
Download or read book Hypersonic Viscous Flow Over Slender Cones written by Lawrence Talbot and published by . This book was released on 1958 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Viscous self-induced pressures on 3 degree-semivertex-angle cones were measured over the range 3.7
Author : Kazimierz J. Orlick-Rückemann
Publisher :
ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.E/5 ( download)
Download or read book Dynamic Viscous Interaction in Hypersonic Flow written by Kazimierz J. Orlick-Rückemann and published by . This book was released on 1970 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 1460 pages
Book Rating : 4.:/5 (31 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 1460 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : Stanley G. Rubin
Publisher :
ISBN 13 :
Total Pages : 85 pages
Book Rating : 4.:/5 (227 download)
Download or read book Hypersonic Viscous Flow Over Slender Bodies Having Sharp Leading Edges written by Stanley G. Rubin and published by . This book was released on 1967 with total page 85 pages. Available in PDF, EPUB and Kindle. Book excerpt: The hypersonic viscous pressure interaction is treated by the development of a set of equations valid throughout the boundary layer, shock-wave structure and inviscid core. Primary interest is concerned with the nature of the leading edge continuum merged layer in which the shock wave and boundary layer are indistinguishable. Due to the parabolic nature of the equations, finite-difference solutions are attainable. The flow over a flat plate at zero incidence, as well as angle of attack, was considered. Velocity and state variable distributions across the viscous layer depict the formation of an outer shock wave and inner constant pressure boundary layer. The calculated values of surface pressure, heat transfer and shock jump conditions were at first significantly below the values predicted by strong interaction theory. Agreement was quite good downstream of the merged layer where Rankine-Hugoniot jump conditions were satisfied to within 8%. (Author).
Author : A. Lin
Publisher :
ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.:/5 (227 download)
Download or read book Three-Dimensional Supersonic Viscous Flow Over a Cone at Incidence written by A. Lin and published by . This book was released on 1981 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: The viscous supersonic flow over a sharp cone at incidence is examined numerically with a coupled strongly implicit algorithm for the properties in the plane normal to the cone axis. The Navier-Stokes equations are considered in a boundary layer-like or parabolized manner and global relaxation is considered for the pressure interaction. It is shown that departure effects can be effectively eliminated by forward differencing for the axial pressure gradient. Moreover, this approximation retains the implicit free pressure interaction required for geometries where axial flow separation is possible. (Author).
