000			01773 a2200217 4500
003			OSt
020			_a9781032245157
040			_cIIT Kanpur
041			_aeng
082			_a629.133 _bSa15a2
100			_aSadraey, Mohammad H.
245			_aAircraft performance [2nd. ed.] _ban engineering approach _cMohammad H. Sadraey
250			_a2nd ed.
260			_bCRC Press _c2024 _aBoca Raton
300			_axxv, 666p
500			_aInstructor and Student Resources
520			_aAircraft Performance: An Engineering Approach, Second Edition introduces flight performance analysis techniques of fixed-wing air vehicles, particularly heavier-than-aircraft. It covers maximum speed, absolute ceiling, rate of climb, range, endurance, turn performance, and takeoff run. Enabling the reader to analyze the performance and flight capabilities of an aircraft by utilizing only the aircraft weight data, geometry, and engine characteristics, this book covers the flight performance analysis for both propeller-driven and jet aircraft. The second edition features new content on vertical takeoff and landing, UAV launch, UAV recovery, use of rocket engine as the main engine, range for electric aircraft, electric engine, endurance for electric aircraft, gliding flight, pull-up, and climb-turn. In addition, this book includes end-of-chapter problems, MATLAB® code and examples, and case studies to enhance and reinforce student understanding. This book is intended for senior undergraduate aerospace students taking courses in Aircraft Performance, Flight Dynamics, and Flight Mechanics. Instructors will be able to utilize an updated Solutions Manual and Figure Slides for their course.
650			_aAirplanes -- Performance
650			_aAerodynamics
942			_cBK
999			_c567335 _d567335