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
General
Is the information for this product incomplete, wrong or inappropriate?
Let us know about it.
Does this product have an incorrect or missing image?
Send us a new image.
Is this product missing categories?
Add more categories.
Review This Product
No reviews yet - be the first to create one!