Product Information
A classic in its field, this university text and reference book has long been one of the basic works. This is the complete reprinting of the revised (1966) edition which brings the subject up to date, including a complete and probably unique chapter on conical flow round sweptback wings.After two introductory chapters on the simplifying assumptions demanded for the study and a final chapter on vectors, the author treats the material in four fairly well-defined parts: (1) two-dimensional aerofoils (two-dimensional motion, rectilinear vortices, the circular cylinder as an aerofoil, Joukowski's transformation, theory of two-dimensional aerofoils, and thin aerofoils); (2) three-dimensional aerofoils (induced velocity, aerofoils of finite aspect ratio, the lifting line theory, lifting surface theory, propellers, and wind tunnel corrections); (3) subsonic and supersonic flow (subsonic flow, supersonic flow, supersonic sweptback and delta wings); and, (4) the aircraft as a whole (simple flight problems, moments, and stability). The treatment is founded on complex variable and vector methods, both of which are explained in the self-contained text. A wealth of problems, illustrations, and cross-references add to the book's value both as a text and a reference. The only prerequisite is a knowledge of the elements of the differential and integral calculus.Product Identifiers
PublisherDover Publications Inc.
ISBN-139780486619804
eBay Product ID (ePID)88299802
Product Key Features
Number of Pages464 Pages
Publication NameTheoretical Aerodynamics
LanguageEnglish
SubjectEngineering & Technology
Publication Year2011
TypeTextbook
AuthorL. M. Milne-Thomson
SeriesDover Books on Aeronautical Engineering
Dimensions
Item Height215 mm
Item Width136 mm
Additional Product Features
Country/Region of ManufactureUnited States
Title_AuthorL. M. Milne-Thomson