Performance graph for a Falcon X Supercharger with a Claudel Hobson A.V.T. Carburetter at 18,000 RPM.
| Identifier | ExFiles\Box 42\3\ Scan053 | |
| Date | 4th December 1936 | |
| FALCON(Aero Engine) X SUPERCHARGER CLAUDEL HOBSON A.V.T. CARBURETTER R.P.M. 18,000 Ⓐ ACROSS S/C Ⓑ ACROSS S/C + CARB. H.P. INPUT EFFICIENCY % PRESSURE RISE INS MERCURY LBS AIR/MIN x------x TOTAL EFFICIENCY = AIR H.P / H.P INPUT o------o ADIABATIC EFFICIENCY = ADIABATIC TEMP. RISE / ACTUAL TEMP. RISE A.A. RUBBRA 4/12/36 | ||
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).