The Aerodynamic Design of Aircraft

The Aerodynamic Design of Aircraft
Author :
Publisher : Pergamon
Total Pages : 584
Release :
ISBN-10 : STANFORD:36105030519917
ISBN-13 :
Rating : 4/5 (17 Downloads)

Book Synopsis The Aerodynamic Design of Aircraft by : Dietrich Küchemann

Download or read book The Aerodynamic Design of Aircraft written by Dietrich Küchemann and published by Pergamon. This book was released on 1978 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt:


The Aerodynamic Design of Aircraft Related Books

The Aerodynamic Design of Aircraft
Language: en
Pages: 0
Authors: Dietrich Küchemann
Categories: Technology & Engineering
Type: BOOK - Published: 2012 - Publisher: AIAA Education

DOWNLOAD EBOOK

Dietrich Kuchemann's The Aerodynamic Design of Aircraft is as relevant and as forward looking today as it was when it was first published in 1978. It comprises
Aircraft Aerodynamic Design with Computational Software
Language: en
Pages: 467
Authors: Arthur Rizzi
Categories: Technology & Engineering
Type: BOOK - Published: 2021-05-20 - Publisher: Cambridge University Press

DOWNLOAD EBOOK

This modern text presents aerodynamic design of aircraft with realistic applications, using CFD software and guidance on its use. Tutorials, exercises, and mini
Aerodynamic Design of Transport Aircraft
Language: en
Pages: 656
Authors: E. Obert
Categories: Science
Type: BOOK - Published: 2009-04-16 - Publisher: IOS Press

DOWNLOAD EBOOK

The origin of Aerodynamic Design of Transport Aircraft stems from the time when the author was appointed part-time professor in the Aerospace Faculty of Delft U
The Aerodynamic Design of Aircraft
Language: en
Pages: 584
Authors: Dietrich Küchemann
Categories: Science
Type: BOOK - Published: 1978 - Publisher: Pergamon

DOWNLOAD EBOOK

Aircraft Aerodynamic Design
Language: en
Pages: 276
Authors: András Sóbester
Categories: Technology & Engineering
Type: BOOK - Published: 2014-11-17 - Publisher: John Wiley & Sons

DOWNLOAD EBOOK

Optimal aircraft design is impossible without a parametric representation of the geometry of the airframe. We need a mathematical model equipped with a set of c