Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking

By H. Tan, Shu Sun, Zhi-Long Yin. 2009

138 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/ad59f692963ea6a548eeb199bd952656c10633bf

How researchers see this paper

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

1. He-xia Huang
2. Shu Sun
3. H. Tan

Citations in the corpus

• Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves (2012, background): “Then, the shock train phenomenon is destroyed and the inlet enters the ‘‘little buzz’’ state as stated by Tan et al. (2009).”