Compressor Stability Enhancement Using Discrete Tip Injection

By K. Suder, M. Hathaway, Scott A. Thorp, A. Strazisar, Michelle B. Bright. 2000

216 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/abc8eadf32b711dab1bce6deb9622a32f8ea7505

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

1. Jen‐Ping Chen
2. Gregory P. Herrick
3. M. Hathaway

Citations in the corpus

• Pre-Stall Behavior of a Transonic Axial Compressor Stage Via Time-Accurate Numerical Simulation (2013, methodology): “Both experimental (Spakovszky et al., 1999 and Suder et al. 2001) and computational studies (Chen et al., 2006, Davis and Yao et al., 2006) indicate the rotating stall of this compressor initiates in the rotor tip region, so the analysis will focus on the rotor tip.”