Airplane Design Part VII: Determination of Stability, Control and Performance Characteristics: Far and Military Requirements

This document was uploaded by one of our users. The uploader already confirmed that they had the permission to publish it. If you are author/publisher or own the copyright of this documents, please report to us by using this DMCA report form.

Simply click on the Download Book button.

Yes, Book downloads on Ebookily are 100% Free.

Sometimes the book is free on Amazon As well, so go ahead and hit "Search on Amazon"

Airplane Design Part VII: Determination of Stability, Control and Performance Characteristics is the seventh book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference. Airplane Design Part VII: Determination of Stability, Control and Performance Characteristics familiarizes the reader with the following fundamentals: - Controllability, maneuverability and trim - Static and dynamic stability - Ride and comfort characteristics - Performance prediction methods - Civil and military airworthiness regulations for airplane performance and stability and control - The airworthiness code and the relationship between failure states, levels of performance and levels of flying qualities

Author(s): Jan Roskam
Series: Airplane Design
Publisher: DARcorporation
Year: 2002

Language: English
Pages: 351
City: Lawrence, KA
Tags: airplane design, aircraft design