Aircraft Performance (PDF)
An Engineering Approach
(Sprache: Englisch)
Aircraft Performance: An Engineering Approach, Second Edition introduces flight performance analysis techniques of fixed-wing air vehicles, particularly heavier-than-air aircraft. It covers maximum speed, absolute ceiling, rate of climb, range, endurance,...
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Aircraft Performance: An Engineering Approach, Second Edition introduces flight performance analysis techniques of fixed-wing air vehicles, particularly heavier-than-air aircraft. It covers maximum speed, absolute ceiling, rate of climb, range, endurance, turn performance, and takeoff run.
Autoren-Porträt von Mohammad H. Sadraey
Dr. Mohammad H. Sadraey is a Professor in the School of Engineering, Technology, and Aeronautics at the Southern New Hampshire University, and the national president of Sigma Gamma Tau honor society. Dr. Sadraey's main research interests are in aircraft design techniques, robust nonlinear control, autopilot, design and automatic control of unmanned air vehicles, and manned-unmanned aircraft teaming. He received his M.Sc. in Aerospace Engineering in 1995 from RMIT, Australia, and his Ph.D. in Aerospace Engineering from the University of Kansas, USA in 2006. Dr. Sadraey is a senior member of the American Institute of Aeronautics and Astronautics (AIAA), and is in Who's Who in America for many years. He has over 26 years of professional experience in academia and industry. Dr. Sadraey is the author of eight textbooks including "Aircraft Design: A Systems Engineering Approach", "Design of Unmanned Aerial Systems", published by Wiley Publications in 2012, and 2019, and Aircraft Performance Analysis by CRC in 2016.
Bibliographische Angaben
- Autor: Mohammad H. Sadraey
- 2023, 2. Auflage, 692 Seiten, Englisch
- Verlag: Taylor & Francis
- ISBN-10: 1000898512
- ISBN-13: 9781000898514
- Erscheinungsdatum: 14.07.2023
Abhängig von Bildschirmgröße und eingestellter Schriftgröße kann die Seitenzahl auf Ihrem Lesegerät variieren.
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- Dateiformat: PDF
- Größe: 21 MB
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Sprache:
Englisch
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