Theoretical Aerodynamics
اپریل 2012 · Courier Corporation
5.0star
2 جائزےreport
ای بک
464
صفحات
reportدرجہ بندیوں اور جائزوں کی تصدیق نہیں کی جاتی ہے مزید جانیں
اس ای بک کے بارے میں
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.
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.
درجہ بندی اور جائزے
5.0
2 جائزے
مصنف کے بارے میں
The late L. M. Milne-Thompson was Emeritus Professor of Applied Mathematics at the University of Arizona and Emeritus Professor of Mathematics in the Royal Naval College. He also taught at Brown University, The University of Wisconsin, and the universities of Rome, Queensland, Calgary, and Otago.
اس ای بک کی درجہ بندی کریں
ہمیں اپنی رائے سے نوازیں۔
پڑھنے کی معلومات
اسمارٹ فونز اور ٹیب لیٹس
Android اور iPad/iPhone.کیلئے Google Play کتابیں ایپ انسٹال کریں۔ یہ خودکار طور پر آپ کے اکاؤنٹ سے سینک ہو جاتی ہے اور آپ جہاں کہیں بھی ہوں آپ کو آن لائن یا آف لائن پڑھنے دیتی ہے۔
لیپ ٹاپس اور کمپیوٹرز
آپ اپنے کمپیوٹر کے ویب براؤزر کا استعمال کر کے Google Play پر خریدی گئی آڈیو بکس سن سکتے ہیں۔
ای ریڈرز اور دیگر آلات
Kobo ای ریڈرز جیسے ای-انک آلات پر پڑھنے کے لیے، آپ کو ایک فائل ڈاؤن لوڈ کرنے اور اسے اپنے آلے پر منتقل کرنے کی ضرورت ہوگی۔ فائلز تعاون یافتہ ای ریڈرز کو منتقل کرنے کے لیے تفصیلی ہیلپ سینٹر کی ہدایات کی پیروی کریں۔
