Rotor 67 mass flow rate, pressure ratio and efficiency experimental values
 

Hi everyone!

I am currently trying to simulate Rotor 67, and later on optimeze it (if possible), by "playing" with sweep and lean on the blade. As final dissertation of my MSc.

Now I am in the process of validating geometry and simulation. In order to do that, I am using NASA Technical Paper 2879, (Anthony J. Strazisar,).

I am unable to find, values of pressure ratio, normalized flow rate and efficiency that are shown in figure 12. Does anyone know how to get them?

Thanks in advance!

Daniel Sanchez-Herranz