Book Description
The plane problem of the vibrating airfoil in supersonic flow is dealt with and solved within the scope of a linearized theory by the method of the acceleration potential.
Author : H. Hönl
Publisher :
Page : 764 pages
File Size : 44,23 MB
Release : 1949
Category : Aerodynamic load
ISBN :
The plane problem of the vibrating airfoil in supersonic flow is dealt with and solved within the scope of a linearized theory by the method of the acceleration potential.
Author : Robert Thomas Jones
Publisher : Princeton University Press
Page : 227 pages
File Size : 24,85 MB
Release : 2014-07-14
Category : Technology & Engineering
ISBN : 1400860776
Originator of many of the theories used in modern wing design, Robert T. Jones surveys the aerodynamics of wings from the early theories of lift to modern theoretical developments. This work covers the behavior of wings at both low and high speeds, including the range from very low Reynolds numbers to the determination of minimum drag at supersonic speed. Emphasizing analytical techniques, Wing Theory provides invaluable physical principles and insights for advanced students, professors, and aeronautical engineers, as well as for scientists involved in computational approaches to the subject. This book is based on over forty years of theoretical and practical work performed by the author and other leading researchers in the field of aerodynamics. Originally published in 1990. 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.
Author :
Publisher :
Page : 434 pages
File Size : 33,83 MB
Release : 1974
Category :
ISBN :
Author : H. Honl
Publisher :
Page : 25 pages
File Size : 43,13 MB
Release : 1947
Category : Aerodynamics, Supersonic
ISBN :
The plane problem of the vibrating wing in supersonic flow is discussed and followed by the acceleration potential method, on the basis of a linearized theory.
Author : United States. Wright Air Development Division
Publisher :
Page : 1268 pages
File Size : 20,50 MB
Release : 1957
Category : Aeronautics
ISBN :
Author : H. Hoenl
Publisher : BiblioGov
Page : 38 pages
File Size : 17,76 MB
Release : 2013-07
Category :
ISBN : 9781289260248
The NASA Technical Reports Server (NTRS) houses half a million publications that are a valuable means of information to researchers, teachers, students, and the general public. These documents are all aerospace related with much scientific and technical information created or funded by NASA. Some types of documents include conference papers, research reports, meeting papers, journal articles and more. This is one of those documents.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 924 pages
File Size : 42,49 MB
Release : 1955
Category : Aeronautics
ISBN :
Author : Holt Ashley
Publisher : Courier Corporation
Page : 306 pages
File Size : 27,28 MB
Release : 1965-01-01
Category : Technology & Engineering
ISBN : 0486648990
This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 274 pages
File Size : 10,59 MB
Release : 1953
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 952 pages
File Size : 42,26 MB
Release : 1987
Category : Aeronautics
ISBN :