Full Newtonian flight model: lift ∝ ½ρV²S·Cl(α), drag = Cd₀ + k·Cl², thrust & weight-inertia, density falloff with altitude, and critical AoA stall. Three airframes, procedural alpine-coastal world, and two mission profiles.
Explore the 12 km terrain. Practice energy management and stalls.
Precision approach to Runway 27L. Manage speed, sink rate & AoA.
High-G pursuit — lead the pipper, manage energy, stay fast.
Rho drops ~10%/1000m. Induced drag rises with Cl². Inertia is rate-limited.