1992-02-01

Flow Measurements at the Inlet of a Turbocharger Turbine 920042

Experiments were conducted at the rotor inlet of a 110 mm turbocharger radial inflow turbine wheel to study the effect of changes in A/R on the flow field entering the rotor. A three-port cobra probe was traversed axially above the rotor tip to obtain velocity triangles at a wide range of operating conditions at each of three different A/R vane settings. In addition, values of the rotor inlet mass average properties are presented.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 43% off list price.
Login to see discount.
Special Offer: Purchase more aerospace standards and aerospace material specifications and save! AeroPaks off a customized subscription plan that lets you pay for just the documents that you need, when you need them.
X