Regime
Set by a stated gust distribution — the average of a curve, not of a flow
Every figure drawn under this hypothesis — 28 of them — with the essay each one belongs to and the generator that drew it.
28 figure placements state this regime. The strip along the foot of every figure names two things — the model that produced it and the regime it holds in — and this listing is read back out of the finished drawing rather than from what produced it.
- One wing root feels the rolling gust its lift cannot — elliptic wing, aspect ratio 9 · gust-average · hero
- One wing root feels the rolling gust its lift cannot — elliptic wing, aspect ratio 9 · gust-average
- One wing root feels the rolling gust its lift cannot — elliptic wing, aspect ratio nine; filters normalised at κ = 0 · gust-average
- One wing root feels the rolling gust its lift cannot — linear, attached; elliptic wing; span b in integral scales L, chord b/9 · gust-average
- One wing root feels the rolling gust its lift cannot — linear, attached; elliptic wing; span b in integral scales L, chord b/9; one root · gust-average
- One wing root feels the rolling gust its lift cannot — linear, attached; elliptic wings of aspect ratio 4 to 100; chord b/9 · gust-average
- One wing root feels the rolling gust its lift cannot — linear, attached; elliptic wing; span b in integral scales L, chord b/9 · gust-average
- The aeroplane rises out of its own gust — stated gust distribution, unsteady thin-aerofoil lift, no pitching, no flexibility · gust-average · hero
- The aeroplane rises out of its own gust — stated gust distribution, unsteady thin-aerofoil lift, no pitching, no flexibility · gust-average
- The aeroplane rises out of its own gust — stated gust distribution, unsteady thin-aerofoil lift, no pitching, no flexibility · gust-average
- The aeroplane rises out of its own gust — stated gust distribution, unsteady thin-aerofoil lift, no pitching, no flexibility · gust-average
- The aeroplane rises out of its own gust — stated gust distribution — 5 m/s peak, two stated aeroplanes at their own speeds · gust-average
- The aeroplane rises out of its own gust — stated gust distribution — standard atmosphere, 0 to 12 km, a stated airliner · gust-average
- The aeroplane rises out of its own gust — stated gust distribution, unsteady thin-aerofoil lift, no pitching, no flexibility · gust-average
- The lift at the mean angle — a stated gust distribution — σ = 3° about 10°, and the wing is quasi-steady · gust-average · hero
- The lift at the mean angle — a stated gust distribution — σ = 3° about 10°, and the wing is quasi-steady · gust-average
- The lift at the mean angle — a stated gust distribution — normal, quasi-steady, and the wing never stalls · gust-average
- The lift at the mean angle — a stated gust distribution — σ = 3° in the linear range, where the lift average is exact · gust-average
- The lift at the mean angle — a stated gust distribution — normal, quasi-steady, and the wing never stalls · gust-average
- The lift at the mean angle — a stated gust distribution — σ = 4° about 13°, and the wing is quasi-steady · gust-average
- The span takes away the infinity, not the gust — a stated gust spectrum — isotropic, frozen, a rigid wing in strip theory · gust-average · hero
- The span takes away the infinity, not the gust — a stated gust spectrum — isotropic, frozen, a rigid wing in strip theory · gust-average
- The span takes away the infinity, not the gust — a stated gust spectrum — isotropic, frozen, a rigid wing in strip theory · gust-average
- The span takes away the infinity, not the gust — a stated gust spectrum — isotropic, frozen, a rigid wing in strip theory · gust-average
- The span takes away the infinity, not the gust — a stated gust spectrum — isotropic, frozen, a rigid wing in strip theory · gust-average
- The span takes away the infinity, not the gust — a stated gust spectrum — isotropic, frozen, a rigid wing in strip theory · gust-average
- The span takes away the infinity, not the gust — a stated gust spectrum — isotropic, frozen, a rigid wing in strip theory · gust-average
- Two lifts at one incidence — a stated gust distribution — σ = 3° about 10°, and the wing is quasi-steady · gust-average