Description / Abstract:
This document discusses formulae considered applicable to
aircraft engines having integral supercharging or directly into the
cylinders. Such engines are normally designated as single and two
speed engines. Correction formulae for engineers having two stage
or exhaust turbo supercharging will not be discussed. Corrections
for engines having a high degree of integral supercharging will be
discussed in general terms only and no specific formulae will be
presented.
The correction formulae and methods listed are empirical and
subject to error due to conditions beyond the scope of known
corrections. Usage has indicated, however, that the correction
formulae listed will provide a satisfactory approximation of power
output under standard conditions.