The four forces, live
The equations with today's numbers
Flight envelope (altitude vs Mach)
Mach limit1.3 g buffet / low-speed limitstall (1 g)thrust ceiling
V-n diagram (load factor vs equivalent airspeed)
Wing section: streamlines and pressure
Lift curve CL(α) with flaps
Drag polar CD = CD0 + k CL2
Self-checks (run in your browser)
The science (and what is simplified)
Equations used
Glossary
About the models