Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Interference Between Wing and Body at Supersonic Speeds: Data report, pressure distribution tests of wing-body interference models at Mach no. of 2.0, phase V tests of August 1951
Author: Aerodynamic Components of Aircraft at High Speeds
Author: Allen F. DonovanPublisher: Princeton University Press
ISBN: 1400879906
Category : Science
Languages : en
Pages : 863
Book Description
Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Wing Theory in Supersonic Flow
Author: Elie CarafoliPublisher: Elsevier
ISBN: 1483160270
Category : Technology & Engineering
Languages : en
Pages : 611
Book Description
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.
High Speed Wing Theory
Author: Doris CohenPublisher: Princeton University Press
ISBN: 1400874947
Category : Technology & Engineering
Languages : en
Pages : 251
Book Description
Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
High Speed Aerodynamics and Jet Propulsion
Author: Allen F. DonovanPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 876
Book Description
AIAA Third International Aerospace Planes Conference: 91-5051 - 91-5104
Author: Subject Index to Unclassified ASTIA Documents
Author: Defense Documentation Center (U.S.)Publisher:
ISBN:
Category : Science
Languages : en
Pages : 296
Book Description
An Experimental Pressure-distribution Investigation of Interference Effects Produced at a Mach Number of 3.11 by Wedge- Shaped Bodies Located Under a Triangular Wing
Author: Lowell E. HaselPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 120
Book Description
Author: S. Kirkby
Author: