Regime
One-dimensional duct flow — the Mach number is the coordinate, not the setting
Every figure drawn under this hypothesis — 53 of them — with the essay each one belongs to and the generator that drew it.
53 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 choke that belongs to two streams — one-dimensional compressible duct; steam, γ = 1.3; 10 °C suction, 130 °C motive; ideal parts · ejector-map · hero
- A choke that belongs to two streams — one-dimensional compressible duct; steam, γ = 1.3; 10 °C suction, 130 °C motive; ideal parts · ejector-map
- A choke that belongs to two streams — A₃/Aₜ = 60, suction at 0.01 of motive; one-dimensional compressible duct; steam, γ = 1.3; 10 °C suction, 130 °C motive; ideal parts · ejector-map
- A choke that belongs to two streams — one-dimensional compressible duct; steam, γ = 1.3; 10 °C suction, 130 °C motive; ideal parts · ejector-map
- A choke that belongs to two streams — one-dimensional compressible duct; steam, γ = 1.3; 10 °C suction, 130 °C motive; ideal parts · ejector-map
- A choke that belongs to two streams — one-dimensional compressible duct: motive steam at 10 bar; γ = 1.3; ideal stages; the intercondensers remove only motive steam · ejector-map
- A choke that belongs to two streams — one-dimensional compressible duct; steam, γ = 1.3; 10 °C suction, 130 °C motive; ideal parts · ejector-map
- A duct that cannot be run backwards — air, constant area, adiabatic · what-a-gas-carries-forward · hero
- A duct that cannot be run backwards — air, constant area, adiabatic · what-a-gas-carries-forward
- A duct that cannot be run backwards — air, constant area, adiabatic · what-a-gas-carries-forward
- A duct that cannot be run backwards — γ = 1.4 · one-dimensional, calorically perfect, adiabatic walls where stated · fanno-rayleigh
- A gas that has not finished being shocked — air, calorically perfect, adiabatic · what-a-gas-carries-forward
- A surface that remembers the diaphragm — air, calorically perfect · what-a-gas-carries-forward
- Friction moves the sonic point past the throat — one-dimensional compressible, Fanno friction with area change — area ratio 2.5, γ = 1.4 · nozzle-duct · hero
- Friction moves the sonic point past the throat — one-dimensional compressible, Fanno friction with area change — area ratio 2.5, γ = 1.4 · nozzle-duct
- Friction moves the sonic point past the throat — one-dimensional compressible, Fanno friction — area ratio 2.5, γ = 1.4 · nozzle-duct
- Friction moves the sonic point past the throat — one-dimensional compressible, Fanno friction — length 0.2, area ratio 2.5, γ = 1.4 · nozzle-duct
- One diaphragm, every wave — p₄/p₁ = 10 · inviscid, one-dimensional, calorically perfect at γ = 1.4 · shock-tube
- One diaphragm, every wave — p₄/p₁ = 40 · inviscid, one-dimensional, calorically perfect at γ = 1.4 · shock-tube
- The nozzle that is best at one thing — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map · hero
- The nozzle that is best at one thing — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The nozzle that is best at one thing — one-dimensional duct, incompressible: the lossless build is a limit; the other uses the borrowed losses · ejector-map
- The nozzle that is best at one thing — one-dimensional duct, incompressible: nozzle loss 0.05; throat and diffuser split evenly in each total · ejector-map
- The nozzle that is best at one thing — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The nozzle that is best at one thing — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The nozzle that is best at one thing — one-dimensional duct, incompressible: borrowed losses as before, one of them removed per curve · ejector-map
- The nozzle that is best at one thing — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The nozzle that is best at one thing — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The shock in a river — Froude 1 to 4, against a γ = 2 gas at the same ratio · hydraulic-jump
- The shock in a river — Froude 1 to 1.4, against a γ = 2 gas at the same ratio · hydraulic-jump
- The theory that forbade flight — β = 30°, γ = 1.4 · inviscid, calorically perfect · newtonian-lift
- The theory that forbade flight — M → ∞ · inviscid, and the gas is calorically perfect at each γ · newtonian-lift
- The theory that forbade flight — β = 10°, γ = 1.4 · inviscid, calorically perfect · newtonian-lift
- The wall the suction puts in the curve — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map · hero
- The wall the suction puts in the curve — R = 0.275, M = 0.92; one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The wall the suction puts in the curve — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The wall the suction puts in the curve — water at 20 °C, pᵥ = 2.34 kPa; R = 0.28; one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The wall the suction puts in the curve — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The wall the suction puts in the curve — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- The wall the suction puts in the curve — one-dimensional duct, incompressible: water at 20 °C; a frictionless suction pipe; losses borrowed as before · ejector-map
- The wall the suction puts in the curve — one-dimensional duct, incompressible; losses 0.05 nozzle, 0.10 suction, 0.10 throat, 0.15 diffuser · ejector-map
- Two totals, one of which a shock cannot touch — air, calorically perfect, adiabatic · what-a-gas-carries-forward · hero
- Two totals, one of which a shock cannot touch — air, calorically perfect, adiabatic · what-a-gas-carries-forward
- Two totals, one of which a shock cannot touch — air, calorically perfect, adiabatic · what-a-gas-carries-forward
- Two totals, one of which a shock cannot touch — air, calorically perfect · what-a-gas-carries-forward
- Two totals, one of which a shock cannot touch — air, calorically perfect, adiabatic · what-a-gas-carries-forward
- Two ways to choke — γ = 1.4 · one-dimensional, calorically perfect · fanno-rayleigh · hero
- Two ways to choke — γ = 1.4 · one-dimensional, calorically perfect · fanno-rayleigh
- Two ways to choke — γ = 1.4 · one-dimensional, calorically perfect, adiabatic walls where stated · fanno-rayleigh
- Two ways to choke — γ = 1.4 · one-dimensional, calorically perfect, adiabatic walls where stated · fanno-rayleigh
- Two ways to choke — M₁ = 2, γ = 1.4 · one-dimensional, calorically perfect · fanno-rayleigh
- Two ways to choke — γ = 1.4 · one-dimensional, calorically perfect · fanno-rayleigh
- Two ways to choke — γ = 1.4 · one-dimensional, calorically perfect · fanno-rayleigh