Infer fluid head from an ideal jet without mixing two heights
For a large open tank with a small opening, compare the free surface and the exiting stream. Both are at atmospheric pressure, and the large surface area makes the surface speed negligible over a short interval. Bernoulli’s equation then gives exit speedv=√(2gh), whereh is the free-surface height above the opening. This is Torricelli’s result under stated ideal assumptions, not a universal discharge rate.
Learning outcome: Vary head at fixed outlet height, then vary outlet height at fixed head. Reconstruct speed and flight time separately before calculating range. Use the assigned range error to bound inferred head; identify a loss mechanism that would bias inference even if repeated ranges were precise.
Starting recap
Review density and unit conversion, perpendicular force components, static force balance, work-energy, mass conservation and projectile motion.
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For head0.60 m,outlet height0.40 m andg10, exit speed√12≈3.464 m/s and flight time√0.08≈0.2828 s. Range is√0.96≈0.9798 m. An assigned range bound±0.01 m gives inferred head limits(R−0.01)²/1.6 and(R+0.01)²/1.6, approximately0.5878 to0.6123 m.
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Does doubling the head double range when outlet height stays fixed?
Experiment
Vary head at fixed outlet height, then vary outlet height at fixed head. Reconstruct speed and flight time separately before calculating range. Use the assigned range error to bound inferred head; identify a loss mechanism that would bias inference even if repeated ranges were precise.
Connect an ideal efflux speed with projectile evidence
Worked teaching model · synthetic values · Large open tank and small horizontal opening, both at the same atmospheric pressure,g10. Surface speed negligible; head approximately constant during a short record. No drag or jet breakup. Assigned horizontal-range uncertainty±0.01 m; exact outlet height. No physical jet or pressurized-vessel activity.
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Axes rescale with settings; compare numerical values, not screen angles or apparent lengths. Solid/points show the selected model relationship or observations; the dashed comparison is explained below.
| Quantity | Value | Unit |
|---|---|---|
| Ideal horizontal exit speed | 3.4641 | m/s |
| Fall time | 0.28284 | s |
| Horizontal range | 0.9798 | m |
| Head inferred from range | 0.6 | m |
| Inferred head lower bound | 0.58782 | m |
| Inferred head upper bound | 0.61231 | m |
Accessible plot coordinates
| horizontal distance (m) | height above landing plane (m) |
|---|---|
| 0 | 0.4 |
| 0.04899 | 0.399 |
| 0.09798 | 0.396 |
| 0.14697 | 0.391 |
| 0.19596 | 0.384 |
| 0.24495 | 0.375 |
| 0.29394 | 0.364 |
| 0.34293 | 0.351 |
| 0.39192 | 0.336 |
| 0.44091 | 0.319 |
| 0.4899 | 0.3 |
| 0.53889 | 0.279 |
| 0.58788 | 0.256 |
| 0.63687 | 0.231 |
| 0.68586 | 0.204 |
| 0.73485 | 0.175 |
| 0.78384 | 0.144 |
| 0.83283 | 0.111 |
| 0.88182 | 0.076 |
| 0.93081 | 0.039 |
| 0.9798 | 0 |
Torricelli’s speed and projectile flight combine to give range2√(head×outlet height).
v=√(2gh) follows equal surface/exit pressure and negligible surface speed. The flight time depends on outlet height, not the head. Inference h=R²/(4y) assumes these conditions; a finite reservoir speed, losses or changing head needs another model.
Torricelli’s speed and projectile flight combine to give range2√(head×outlet height).
v=√(2gh) follows equal surface/exit pressure and negligible surface speed. The flight time depends on outlet height, not the head. Inference h=R²/(4y) assumes these conditions; a finite reservoir speed, losses or changing head needs another model.
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What observation could challenge the assumption that surface speed is negligible?
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