Airplane Design Part VII: Determination of Stability, Control and Performance Characteristics: Far and Military Requirements
Airplane Design Part VII: Determination of Stability, Control and Performance Characteristics: Far and Military Requirements By Jan Roskam
2002 | 351 Pages | ISBN: 1884885101 | PDF | 25 MB
2002 | 351 Pages | ISBN: 1884885101 | PDF | 25 MB
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