November 2015
Intermediate to advanced
647 pages
21h 38m
English

The aspect ratio A of the wing is the ratio of the area of a square whose side is the span b to the actual planform area of the wing, denoted by S:
(7.128)
The Mach number enters Eqn (7.127) through the subsonic form of the Prandtl–Glauert factor
(7.129)
If the ...