Research Article
Combustion Characteristics in Rotating Detonation Engines
Figure 8
Pressure traces obtained by S1 and S2 for the air mass flow rate 636 g/s and short-time Fourier transform for the pressure trace S1.
(a) Global view |
(b) Transient phase, unstable SRDW |
(c) Steady phase, SRDW |
(d) Short-time Fourier transform |