Skip to main content

Currently Skimming:


Pages 74-76

The Chapter Skim interface presents what we've algorithmically identified as the most significant single chunk of text within every page in the chapter.
Select key terms on the right to highlight them within pages of the chapter.


From page 74...
... 74 Exhaust Emissions from In-Use General Aviation Aircraft wall is less than the gas, which is often the case when engine exhaust is sampled. Particle loss due to turbulent diffusion is the largest size-dependent loss where the loss is highest for the smallest particles.
From page 75...
... Figure I-2. Predicted Particle Losses for Campaign 1 and 2 (top plot)
From page 76...
... 76 Many of the aircraft measured for ACRP Project 02-54 engine tests had no fuel flow gauge. Furthermore, aircraft with analog fuel flow gauges as opposed to digital gauges often do not register fuel flow at idle (dial is below the lowest mark)

Key Terms



This material may be derived from roughly machine-read images, and so is provided only to facilitate research.
More information on Chapter Skim is available.