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Bound And Trailing Vortices In The Linearised Theory Of Supersonic Flow And The Downwash In The Wake Of A Delta Wing
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Author :Arthur ROBINSON (M.Sc., A.F.R.Ae.S., and TOD (Sir John Hunter Hunter) K.B.E.) Publisher : ISBN 13 : Total Pages : pages Book Rating :4.:/5 (54 download)
Book Synopsis Bound and Trailing Vortices in the Linearised Theory of Supersonic Flow, and the Downwash in the Wake of a Delta Wing by : Arthur ROBINSON (M.Sc., A.F.R.Ae.S., and TOD (Sir John Hunter Hunter) K.B.E.)
Download or read book Bound and Trailing Vortices in the Linearised Theory of Supersonic Flow, and the Downwash in the Wake of a Delta Wing written by Arthur ROBINSON (M.Sc., A.F.R.Ae.S., and TOD (Sir John Hunter Hunter) K.B.E.) and published by . This book was released on 1952 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bound and trailing Vortices in the linearised theory of supersonic flow, and the downwash in the wake of a delta wing by : A. Robinson
Download or read book Bound and trailing Vortices in the linearised theory of supersonic flow, and the downwash in the wake of a delta wing written by A. Robinson and published by . This book was released on 1952 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bound and Trailing Vortices in the Linearised Theory of Supersonic Flow, and the Downwash in the Wake of a Delta Wing by : Arthur Taylor
Download or read book Bound and Trailing Vortices in the Linearised Theory of Supersonic Flow, and the Downwash in the Wake of a Delta Wing written by Arthur Taylor and published by . This book was released on 1950 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bound and Trailing Vortices in the Linearised Theory of Supersonic Flow, and the Downwash in the Wake of a Delta Wing by : Aeronautical Research Council
Download or read book Bound and Trailing Vortices in the Linearised Theory of Supersonic Flow, and the Downwash in the Wake of a Delta Wing written by Aeronautical Research Council and published by . This book was released on 1952 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bound and Trailing Vortices in the Linearised Theory of Supersonic Flow, and the Downwash in the Wake of a Delta Wing by :
Download or read book Bound and Trailing Vortices in the Linearised Theory of Supersonic Flow, and the Downwash in the Wake of a Delta Wing written by and published by . This book was released on 1947 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wing Theory in Supersonic Flow by : Elie Carafoli
Download or read book Wing Theory in Supersonic Flow written by Elie Carafoli and published by Elsevier. This book was released on 2013-10-22 with total page 611 pages. Available in PDF, EPUB and Kindle. Book excerpt: Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the characteristics of drag, lift, and moments for various shapes of the trailing edge line. This book discusses as well the wings of ordinary shapes, delta wings, yawed wings, polygonal wings, trapezoid wings, and arrow-head or swept-back wings. The final chapter deals with a delta wing with a central fusiform body. This book is a valuable resource for teachers, students, and specialists engaged in modern aerodynamics.
Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 886 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Method for Calculating Downwash Field Due to Lifting Surfaces at Subsonic and Supersonic Speeds by : Sidney M. Harmon
Download or read book Method for Calculating Downwash Field Due to Lifting Surfaces at Subsonic and Supersonic Speeds written by Sidney M. Harmon and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method utilizing source singularities is presented for obtaining the linearized downwash field due to lifting wings at subsonic and supersonic speeds. The method is applied to derive generalized formulas for the downwash field due to uniformly loaded swept and rectangular wings at subsonic and supersonic speeds. The utilization of these formulas to obtain the downwash due to wings of arbitrary loading is indicated.
Book Synopsis Aerodynamic Loads on a Leading-edge Flap and a Leading-edge Slat on the NACA 64A010 Airfoil Section by : John A. Kelly
Download or read book Aerodynamic Loads on a Leading-edge Flap and a Leading-edge Slat on the NACA 64A010 Airfoil Section written by John A. Kelly and published by . This book was released on 1954 with total page 706 pages. Available in PDF, EPUB and Kindle. Book excerpt: A previous report, NACA TN 3007, gave force and moment data for the NACA 64A010 airfoil section equipped alternately with a flap and a slat at the leading edge, and with a split flap and a double-slotted flap at the trailing edge. The present report presents the chordwise distributions of pressure measured concurrently with the force and moment data of NACA 3007. The pressure data for the leading-edge flap and slat have been converted into coefficients of normal force, chord force, and moment based on the geometry of the leading-edge device.
Book Synopsis Linearized Theory of Steady High-Speed Flow by : G. N. Ward
Download or read book Linearized Theory of Steady High-Speed Flow written by G. N. Ward and published by Cambridge University Press. This book was released on 2016-02-25 with total page 261 pages. Available in PDF, EPUB and Kindle. Book excerpt: Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Book Synopsis Aerodynamic Investigation at Mach Number 1.92 of a Rectangular Wing and Tail and Body Configuration and Its Components by : Macon C. Ellis
Download or read book Aerodynamic Investigation at Mach Number 1.92 of a Rectangular Wing and Tail and Body Configuration and Its Components written by Macon C. Ellis and published by . This book was released on 1950 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation at Mach number 1.92 in the Langley 9-inch supersonic tunnel of a variable body-wing-tail configuration has been made in order to determine and to isolate the aerodynamic effects on each other of the components of the configuration.
Book Synopsis A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds by : John C. Martin
Download or read book A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds written by John C. Martin and published by . This book was released on 1954 with total page 720 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical investigation is presented of the contribution of horizontal tails to the lift and pitching moment due to angle of attack, a constant rate of pitch, and a constant vertical acceleration. Numerical values of the aerodynamic coefficients associated with these motions are presented for a number of two-dimensional wing-tail combinations, a triangular wing-tail combination, and a number of rectangular-wing - triangular-tail combinations.
Download or read book Technical Note written by and published by . This book was released on 1952 with total page 570 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Memorandum written by and published by . This book was released on 1958 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis WADC Technical Report by : United States. Wright Air Development Division
Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1957 with total page 1268 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Method for Determining the Frequency-response Characteristics of an Element of System from the System Transient Output Response to a Known Input Function by : Charles W. Matthews
Download or read book Method for Determining the Frequency-response Characteristics of an Element of System from the System Transient Output Response to a Known Input Function written by Charles W. Matthews and published by . This book was released on 1950 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Memorandum by : United States. National Aeronautics and Space Administration
Download or read book NASA Memorandum written by United States. National Aeronautics and Space Administration and published by . This book was released on 1959 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt:
