2024 journal article

Rotating detonation combustor operability and aero-thermal performance with an integrated diverging nozzle

APPLIED THERMAL ENGINEERING, 249.

By: J. Braun* & G. Paniagua *

author keywords: Non-premixed rotating detonation combustors with short diverging nozzles; Subsonic to supersonic operability; Convective heat flux; Injector dynamics
Source: Web Of Science
Added: July 1, 2024