Steady Aircraft Flight and Performance / / N. Harris McClamroch.

• Superior document: Title is part of eBook package: De Gruyter Princeton University Press eBook-Package Backlist 2000-2013
• VerfasserIn: McClamroch, N. Harris,
• Place / Publishing House: Princeton, NJ : : Princeton University Press, , [2011]; ©2011
• Year of Publication: 2011
• Language: English
• Physical Description: 1 online resource (416 p.) :; 23 halftones. 70 line illus.
• Other title: Frontmatter --; CONTENTS --; LIST OF ILLUSTRATIONS --; LIST OF MATLAB M-FILES --; PREFACE --; 1. Aircraft Components and Subsystems --; 2. Fluid Mechanics and Aerodynamics --; 3. Aircraft Translational Kinematics, Attitude, Aerodynamic Forces and Moments --; 4. Propulsion Systems --; 5. Prelude to Steady Flight Analysis --; 6. Aircraft Steady Gliding Longitudinal Flight --; 7. Aircraft Cruise in Steady Level Longitudinal Flight --; 8. Aircraft Steady Longitudinal Flight --; 9. Aircraft Steady Level Turning Flight --; 10. Aircraft Steady Turning Flight --; 11. Aircraft Range and Endurance in Steady Flight --; 12. Aircraft Maneuvers and Flight Planning --; 13. From Steady Flight to Flight Dynamics --; Appendix A. The Standard Atmosphere Model --; Appendix B. End-of-Chapter Problems --; REFERENCES --; INDEX
• Format: Mode of access: Internet via World Wide Web.
• ISBN: 9781400839063; 9783110442502
• DOI: 10.1515/9781400839063?locatt=mode:legacy
• Access: restricted access
• Hierarchical level: Monograph
• Statement of Responsibility: N. Harris McClamroch.

This undergraduate textbook offers a unique introduction to steady flight and performance for fixed-wing aircraft from a twenty-first-century flight systems perspective. Emphasizing the interplay between mathematics and engineering, it fully explains the fundamentals of aircraft flight and develops the basic algebraic equations needed to obtain the conditions for gliding flight, level flight, climbing and descending flight, and turning flight. It covers every aspect of flight performance, including maximum and minimum air speed, maximum climb rate, minimum turn radius, flight ceiling, maximum range, and maximum endurance. Steady Aircraft Flight and Performance features in-depth case studies of an executive jet and a general aviation propeller-driven aircraft, and uses MATLAB to compute and illustrate numerous flight performance measures and flight envelopes for each. Requiring only sophomore-level calculus and physics, it also includes a section on translational flight dynamics that makes a clear connection between steady flight and flight dynamics, thereby providing a bridge to further study. Offers the best introduction to steady aircraft flight and performance Provides a comprehensive treatment of the full range of steady flight conditions Covers steady flight performance and flight envelopes, including maximum and minimum air speed, maximum climb rate, minimum turn radius, and flight ceiling Uses mathematics and engineering to explain aircraft flight Features case studies of actual aircraft, illustrated using MATLAB Seamlessly bridges steady flight and translational flight dynamics