Chemical potential difference → Mechanical work
Chemical potential differenceCombustionTemperature gradientMarangoni effectFluid flowAerodynamic and hydrodynamic liftMechanical motionMechanical work
Epistemic state of the route
- known constituent relations
- 7 / 7 established or replicated · weakest constituent established
- constituent maturity floor
- K4 · experimentally observed
- search for this exact route
- Not assessed — complete composition not searched.
- recorded-pathway overlap
- none recorded
- route-level evidence
- 0 sources for the complete composition · 5 cited by the constituent steps
- boundaries and interfaces
- BOUNDARY compatible · no region transition
Explorematrix context · physics checks · steps · route evidence · constituent evidence · cite
Matrix context
D = disequilibrium row · C = coupling family column. A cell reads the state of the atlas for that pair.
D.05 × C.29 · Chemical potential difference × Thermochemicalfamily: ThermochemicalD.05 × C.34 · Chemical potential difference × Marangonifamily: MarangoniD.05 × C.24 · Chemical potential difference × Turbomachineryfamily: Turbomachinery
Typed bounds on this route
Every limit the atlas holds for this route, as constraint records: reached through bounded_by claims on the route's own entities. Hard bounds (an upper bound or a formula) decide the thermodynamic-bound check above; benchmarks, constitutive relations and resource limits are listed and never decisive. No prose limit exists anywhere (pass 42).
- Carnot limit · formula-bound · hard, applies to this routeη ≤ 1 − T_c/T_h for any heat engine between reservoirs at T_h and T_c
- Betz limit · upper-bound · hard, filtered out by its applicabilityC_p ≤ 16/27 ≈ 59.3% of the kinetic power through the rotor disc
Steps
- 01chemical → thermal · loss to radiative
- fuel, oxidiser and an ignition source; flame temperature 1500–2500 K
gas · above ~700 Krefs [1] - 02
- 03thermal → kinetic · loss to thermal
- thermocapillary case: surface tension falls with temperature, so a temperature gradient along the interface drives flow toward the cold side
liquid · temperature gradient requiredrefs [2] [3] - 04
- 05kinetic → mechanical · loss to thermal
- a rotor or vane in the produced stream at a working angle of attack; the driven flow must carry a directed momentum flux for a blade to load
bulk flow requiredrefs [4] [5] - 06mechanical → mechanicalrefs [5]
- 07mechanical → mechanical · loss to thermalrefs [1]
Evidence for the complete composition · 0
No source on record for this exact composition. The sources below support the individual steps, not the route as a whole.
Evidence for the constituent relations · 5
- [1]A. Bejan. Advanced Engineering Thermodynamics (4th ed.) (2016)
- [2]L. E. Scriven, C. V. Sternling. The Marangoni Effects (1960)
- [3]Q. Dai et al.. Directional interfacial motion of liquids: Fundamentals, evaluations, and manipulation strategies (2021)
- [4]A. Betz. Das Maximum der theoretisch möglichen Ausnützung des Windes durch Windmotoren (1920)
- [5]S. L. Dixon, C. A. Hall. Fluid Mechanics and Thermodynamics of Turbomachinery (7th ed.) (2014)
Cite this route
Physical Transformation Atlas (2026). route p-2543832cd0: Chemical potential difference → Combustion → Temperature gradient → Marangoni effect → Fluid flow → Aerodynamic and hydrodynamic lift → Mechanical motion → Mechanical work. Dataset revision rbfbfcbb70e57 (hash of the canonical data). https://physical-transformation-atlas.wldud5192.workers.dev/path/2543832cd0
Ids and matrix addresses are stable across revisions; the revision hash identifies the exact canonical files the record was compiled from and is meta.data_hash in every /api export. Reuse terms: see the license field in any export.