System Performance and Thermodynamic Cycle Analysis of Airbreathing Pulse Detonation Engines

By Yuhui Wu, Fuhua Ma, Vigor Yang. 2003

154 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/f5edb4e454e7edb42261c6e3787ac74b3e8b7f68

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. Jeong-Yeol Choi
2. Fuhua Ma
3. Vigor Yang
4. Frank K. Lu
5. Eric M. Braun
6. D. Wilson
7. José Camberos

In Mechanics of Materials

1. Jeong-Yeol Choi
2. Fuhua Ma
3. Vigor Yang
4. Frank K. Lu
5. Eric M. Braun
6. D. Wilson
7. José Camberos

Citations in the corpus

• Propulsive performance of airbreathing pulse detonation engines (2006, methodology): “Although not strictly proved, a CD nozzle appears to bemore suited for PDEs than other configurations because of the advantages of preserving the chamber pressure during the blowdown and filling processes and providing more thrust surface area during the exhaust of detonation products [3,17,18,24].”
• Airbreathing rotating detonation wave engine cycle analysis (2010, background): “1 and an altitude of 9300 m [40].”