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From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).
High compression engine test data sheet detailing thermal efficiency, power output, and heat balance.

Identifier  ExFiles\Box 24\4\  Scan091
Date  6th September 1923 guessed
  
SHEET 1. HIGH COMPRESSION.

THERMAL EFFICIENCY, POWER ETC. OF 40/50 HP. RR TEST ENGINE.
COMPRESSION RATIO 4.4.
FUEL "SHELL" NO.2. S.G. .752. CAL.{Mr Calvert} VALUE (LOWER) 19.000 B.Th.U's/LB.

| R.P.M. | Fuel pts. hr. | Pts. HP. hr. | B.H.P. | I.H.P. | HP. to drive motor. | Temp. Jacket water. oC Inlet. Outlet. | Lbs. water to jacket min. | B.Th.U's. to jacket water. | Mech.Effcy. |
|---|---|---|---|---|---|---|---|---|---|
| 500 | 18 | .76 | 23.6 | 27.6 | 4 | 60 | 74 | 68.05 | 1714.3 | 85.5% |
| 750 | 27 | .76 | 35.3 | 40.8 | 5.5 | 63 | 75 | 92.34 | 1994.5 | 86.5% |
| 1000 | 34 | .72 | 47.3 | 55.3 | 8 | 66 | 77 | 120.5 | 2385.9 | 85.6% |
| 1250 | 44 | .73 | 59.6 | 71.1 | 11.5 | 66.5 | 77.5 | 149.1 | 2952.2 | 83.8% |
| 1500 | 49 | .69 | 70.3 | 85.8 | 15.5 | 70 | 81 | 180.4 | 3571.9 | 82.0% |
| 1750 | 56.5 | .74 | 76.2 | 96.2 | 20 | 72 | 81 | 220.9 | 3578.6 | 79.3 |
| 2000 | 59 | .71 | 82.5 | 108.5 | 26 | 73.5 | 82 | 255 | 3901.5 | 76.0 |

HEAT BALANCE

| | R.P.M. | | | |
|---|---|---|---|---|
| | 500 | 1000 | 1500 | 2000 |
| Thermal equt. work done. | | 1000 | 2005 | 2983 | 3499 |
| Loss to engine friction. | | 169 | 339 | 636 | 1103 |
| Heat loss to jackets. | | 1715 | 2386 | 3572 | 3901 |
| Loss through exhaust radiation etc. (By difference) | | 2774 | 5400 | 7399 | 9067 |
| Heat supplied. | 5508 | 10130 | 14590 | 17570 |

SHEET 1. CONTD:-
  
  


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