Regime
Ma near 1 — transonic
Every figure drawn under this hypothesis — 27 of them — with the essay each one belongs to and the generator that drew it.
27 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.
- A free waist needs half the depth, and the sweep costs it nothing — Ma 0.8; spheroid of fineness ten; root chord 0.15 of the length; strip to one fuselage radius outboard · sphere-flow · hero
- A free waist needs half the depth, and the sweep costs it nothing — Ma 0.8; spheroid of fineness ten; root chord 0.15 of the length; strip to one fuselage radius outboard · sphere-flow
- A free waist needs half the depth, and the sweep costs it nothing — unswept root; Ma 0.8; fineness ten · sphere-flow
- A free waist needs half the depth, and the sweep costs it nothing — Ma 0.8; spheroid of fineness ten; root chord 0.15 of the length; strip to one fuselage radius outboard · sphere-flow
- A free waist needs half the depth, and the sweep costs it nothing — Ma 0.8; spheroid of fineness ten; root chord 0.15 of the length; strip to one fuselage radius outboard · sphere-flow
- A free waist needs half the depth, and the sweep costs it nothing — Ma 0.8; spheroid of fineness ten; root chord 0.15 of the length; strip to one fuselage radius outboard · sphere-flow
- A free waist needs half the depth, and the sweep costs it nothing — Ma 0.8; spheroid of fineness ten; root chord 0.15 of the length; strip to one fuselage radius outboard · sphere-flow
- A free waist needs half the depth, and the sweep costs it nothing — Ma 0.8; spheroid of fineness ten; root chord 0.15 of the length; strip to one fuselage radius outboard · sphere-flow
- A waist moves the overspeed and cannot remove it — subsonic, Ma 0.8 unless stated; fineness ten, root chord 0.15 of the fuselage's length · sphere-flow · hero
- A waist moves the overspeed and cannot remove it — subsonic, Ma 0.8 unless stated; fineness ten, root chord 0.15 of the fuselage's length · sphere-flow
- A waist moves the overspeed and cannot remove it — subsonic, Ma 0.8 unless stated; fineness ten, root chord 0.15 of the fuselage's length · sphere-flow
- A waist moves the overspeed and cannot remove it — subsonic, Ma 0.8 unless stated; fineness ten, root chord 0.15 of the fuselage's length · sphere-flow
- A waist moves the overspeed and cannot remove it — subsonic, Ma 0.8 unless stated; fineness ten, root chord 0.15 of the fuselage's length · sphere-flow
- A waist moves the overspeed and cannot remove it — subsonic, Ma 0.8 unless stated; fineness ten, root chord 0.15 of the fuselage's length · sphere-flow
- A waist moves the overspeed and cannot remove it — subsonic, Ma 0.8 unless stated; fineness ten, root chord 0.15 of the fuselage's length · sphere-flow
- The wing the equation is really solving — linearised compressible flow at Ma = 0.85 · thin section, small disturbance · shape-from-pressure
- What a signal travels at — Ma 0.90 to 0.90 — no cone below one · sound-signal
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle · hero
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle
- Matched at one speed and at no other — compressible mean line, γ = 1.4 — first-rotor relative Ma ≈ 1.01 at design, losses in a stated efficiency · velocity-triangle
- The only law that forbids it — Ma 1.05 in front — supersonic, γ = 1.4 · normal-shock