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Author : Brown University. Division of Engineering
Publisher :
ISBN 13 :
Total Pages : 106 pages
Book Rating : 4.E/5 ( download)
Download or read book Reverse Flow and Supersonic Interference written by Brown University. Division of Engineering and published by . This book was released on 1958 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Joseph Henry Clarke
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.E/5 ( download)
Download or read book Reverse-flow Integral Methods for Second-order Supersonic Flow Theory written by Joseph Henry Clarke and published by . This book was released on 1963 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: A general reverse-flow relation is obtained within the framework of second-order (in surface deflection) supersonic flow theory. From this it is shown that the second-order increment in the drag of an arbitrary quasicylindrical body can be expressed as surface and volume integrals of the first-order solutions corresponding to forward and reverse flow past the body. Analogous results are obtained for second-order transverse forces and moments on an arbitrary quasiplanar wing, except the first-order reverse flow must correspond to certain zero-thickness wings. Other similar results are possible. Thus, second order aerodynamic forces on bodies may be obtained from first-order solutions by quadrature. It is also shown that the reverse-flow integral relation can yield the pressure distribution on the surface by inversion of an integral equation constructed therefrom. It is thought that these results should be particularly useful for the Mach number range between that of linearized theory and that of full hypersonic small-disturbance theory. (Author).
Author : Zegmund O. Bleviss
Publisher :
ISBN 13 :
Total Pages : 446 pages
Book Rating : 4.:/5 (52 download)
Download or read book Interference Effects in Supersonic Flow written by Zegmund O. Bleviss and published by . This book was released on 1951 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Joseph Henry Clarke
Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.E/5 ( download)
Download or read book Uniform Second-order Solution for Supersonic Flow Over Delta Wing Using Reverse-flow Integral Method written by Joseph Henry Clarke and published by . This book was released on 1963 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of supersonic flow over an inclined flatplate delta wing with supersonic edges is solved to second order in incidence. This solution for surface pressure is uniform and fully analytic. The approach utilizes a reverse-flow integral method previously developed for secondorder problems. This method is augmented by a number of techniques appropriate to its framework. The simplification over standard techniques acgieved by using these reverse-flow methods is quite substantial and makes the problem tractible. Reverse-flow procedures give a volume-surface integral relation that connects the second-order forward flow over the body of interest with the linearized reverse-flow over a related body. A singular integral equation is generated from the integral relation by introducing the edge sweep of the reverse-flow wing as a free parameter. An inversion is available which gives the second-order solution on the surface of the wing. The solution is then made uniformly valid using techniques previously developed. (Author).
Author : Vernon Albert Lee
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (393 download)
Download or read book Interference effects from total-pressure rakes in supersonic flow written by Vernon Albert Lee and published by . This book was released on 1955 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John E. Burkhalter
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.3/5 (91 download)
Download or read book Aerodynamic Interference of Two Axisymmetric Stores at Low Supersonic Speeds written by John E. Burkhalter and published by . This book was released on 1976 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method for determining the basic pressure distribution on an axisymmetric body in supersonic flow has been evaluated. Supersonic line sources with linearly varying strengths placed along the centerline of the body were used to generate the body shape. The results of these theoretical computations for an isolated body agreed very well with experimental data. Two approaches were investigated to determine the pressure distribution on two bodies interfering with each other. In the first approach supersonic point sources were placed along an image line, as determined by subsonic theory, and along the body centerline. The strengths of these point sources were determined so that body boundary conditions were met on top and bottom of each interfering body. Computational problems were encountered with this techniuqe resulting from the nature of induced velocities from a supersonic point source and the approach was finally abandoned. The second interference approach utilized linearly varying line sources placed along an image line and along the body centerline. The location of the image line is solely a function of the delta-x interval chosen for the problem. As before, body boundary conditions were met on top and on bottom of each interfering body. The results of these computations appear realistic for thin bodies.
Author : K. Stewartson
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (11 download)
Download or read book On Wing-body Interference in Supersonic Flow written by K. Stewartson and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Marten T. Landahl
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (32 download)
Download or read book The Interference Between Two Intersecting Perpendicular Two-dimensional Supersonic Flow Fields written by Marten T. Landahl and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Henry Portnoy
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (93 download)
Download or read book Some interference problems in linearised supersonic flow written by Henry Portnoy and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael Chen-Chiang Fong
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (532 download)
Download or read book The Wing-body Interference Problem for Linearized Supersonic Flow written by Michael Chen-Chiang Fong and published by . This book was released on 1953 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Roland Duane Jenison
Publisher :
ISBN 13 :
Total Pages : 130 pages
Book Rating : 4.:/5 (373 download)
Download or read book Foreplane-wing Interference Effects in Supersonic Flow written by Roland Duane Jenison and published by . This book was released on 1965 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 814 pages
Book Rating : 4.:/5 (26 download)
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1968 with total page 814 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : A. F. Charwat
Publisher :
ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (224 download)
Download or read book Supersonic Interference Flow Along the Corner of Intersecting Wedges written by A. F. Charwat and published by . This book was released on 1966 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the inviscid supersonic flow field in a corner formed by two intersecting wedges is reported. The study includes measurements of the distribution of the surface pressure and the wave structure of the flow field in the corner region both for a symmetrical corner configuration (e. e., equal wedge angles) in the Mach-number range between 2.5 and 4 and for an asymmetrical model at one Mach number as a function of the incidence angle of one wedge. A clearly identifiable shock structure is discovered that divides the interference field into four zones. The total extent of the disturbance near the surfaces of the model is approximately twice the extent indicated by available small-perturbation analyses. The highest pressure rise occurs in the inner zone near the corner; the magnitude of this rise is related successfully to the second-order linearized theory. The inviscid flow field is shown to involve strong cross-stream pressure and entropy gradients both at the corner proper and away from it, which cannot be disregarded in analyses of the viscous boundary layer. (Author).
Author : United States. Air Force. Office of Scientific Research
Publisher :
ISBN 13 :
Total Pages : 1136 pages
Book Rating : 4.3/5 (243 download)
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:
Author : Eugene S. Love
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.3/5 (126 download)
Download or read book A Summary of Information on Support Interference at Transonic and Supersonic Speeds written by Eugene S. Love and published by . This book was released on 1954 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: A compilation of available information on the problem of support interference at transonic and supersonic speeds is presented.
Author : David S. Scott
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (245 download)
Download or read book Evidence of Supersonic Reverse Flow Behind the Reflected Wave in an Electromagnetic Shock Tube written by David S. Scott and published by . This book was released on 1968 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Shinya Kobayakawa
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (298 download)
Download or read book Interference of Body and Trailing Edge Vortex Sheet in Supersonic Flow written by Shinya Kobayakawa and published by . This book was released on 1959 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
