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Preferred for those specifically focused on General Aviation due to its modern, deep, and meticulous focus on light aircraft. Editions and Availability
It uses an "equation/derivation/solved example" format. The 2nd edition further separates these elements using shaded regions to improve readability. general aviation aircraft design snorri gudmundsson pdf
Longitudinal static stability: choose wing mean aerodynamic chord (MAC) and position CG ahead of aerodynamic center. Typical tail volume coefficient: Vh = (lh × Sh) / (c × S) where lh = tail moment arm (distance CG to tail AC), c = MAC. Preferred for those specifically focused on General Aviation