Mixing and combustion studies using cavity-based flameholders in a supersonic flow

By M. Gruber, J. Donbar, C. Carter, K. Hsu. 2004

374 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/6860add634f66f8e0d56db31a8193bb24d8fc480

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. Zhenguo Wang
2. Hong-bo Wang
3. Mingbo Sun

In Computational Mechanics

1. Hong-bo Wang
2. Mingbo Sun
3. Zhenguo Wang

Citations in the corpus

• Review of cavity-stabilized combustion for scramjet applications (2014, background): “Gruber et al.31 compared the cavity-stabilized combustion with various fuel injection schemes and found that direct cavity fuel injection was better than passive injection for providing a spatially uniform fuel-air mixture and for maintaining a stable flame during the ignition transient.”