Propulsive Performance of a Continuously Rotating Detonation Engine

By T. Yi, Jing Lou, C. Turangan, Jeong-Yeol Choi, P. Wolański. 2011

203 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Safety, Risk, Reliability and Quality, Statistics and Probability

View Paper: https://www.semanticscholar.org/paper/9222900dec0284f4614f157786b1a7ea657ae888

How researchers see this paper

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

In Aerospace Engineering

1. Frank K. Lu
2. Eric M. Braun
3. D. Wilson
4. José Camberos

In Statistics and Probability

1. Frank K. Lu
2. Eric M. Braun
3. D. Wilson

Citations in the corpus

• Rotating detonation wave propulsion: Experimental challenges, modeling, and engine concepts (2014, unknown): “Computational studies presented thus far have typically used premixed reactants [69,70].”
• Airbreathing rotating detonation wave engine cycle analysis (2010, background): “0 [15,34,41], so fixing the exit Mach number at 1.”