Retro
Aerospace
- Oct 30, 2006
- 8
Looking for formulas to calculate the inlet diffuser efficiency. Given the inlet cross section area and diffuser exit cross section area including the temp, velocity, and density of the free stream what would the results be at the diffuser exit? How much does the velocity decrease? How much do the density, temp and pressure increase? What are the characteristics of the air entering the combustion chamber?