A reference for engineers and students, this volume devotes more than 300 pages to theoretical and experimental considerations. It progresses from elementary materials to methods used in the design of NACA low-drag airfoils, and it presents techniques for using wing-section data to predict wing characteristics. Requires differential and integral calculus and elementary mechanics. 1949 edition.
Corrected reprint of the 1st (1949) edition, with a new preface by the authors.
|Availability||Usually ships in 24 to 48 hours|
|Author/Editor||Ira H. Abbott, A. E. von Doenhoff|
|Dimensions||5 3/8 x 8 1/2|