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Articles

Optical Measurement of Fluid Motion in Semi-Valveless Pulse Detonation Combustor with High-Frequency Operation

, , , , , & show all
Pages 197-212 | Received 20 Aug 2018, Accepted 13 Dec 2018, Published online: 25 Dec 2018
 

ABSTRACT

The purge layer of a semi-valveless pulse detonation cycle (PDC) needs to be minimized for operating at a gas-dynamic upper frequency limit. Therefore, it is essential to better understand the process of burned gas backflow for minimizing the purge layer thickness. The flow field of the semi-valveless PDC was visualized to illustrate the movement of burned gas. A combustor of length of 95 mm with a 10-mm-square cross section was used. Supercritical ethylene and oxygen gas were used as fuel and oxidizer, respectively, and the operation frequency was 604 Hz. The unsteady refilling process of the detonable mixture was modeled by an isentropic flow. In addition, the detailed burned gas blowdown process with deflagration-to-detonation transition (DDT) and the backflow were captured. It was shown that the retonation wave generated by the DDT process was the primary trigger of the burned gas backflow. When the duration required for the DDT process was sufficiently shorter than that of the burned gas blowdown process, it was found the latter could be reproduced with approximately 90% accuracy by one-dimensional numerical analysis without the DDT process.

Nomenclature

A=

speed of sound

A=

cross-sectional area

cp=

specific heat at constant gas pressure

DCJ=

Chapman–Jouguet detonation speed

ER=

equivalence ratio of detonable mixture

fope=

operating frequency

fupper=

upper limit frequency

Id=

inner diameter

Lc=

length of combustor

=

mass flow rate

P=

pressure

R=

gas constant

T=

temperature

tDDT=

time to DDT occurrence from ignition time

tspark=

time to ignition from starting fuel injection

Δtexhaust=

duration to exhaust burned gas from exhaust detonation wave

Δtcycle=

duration of one cycle

Δtinj=

duration of fuel injection

Δtpurge=

duration of purging burned gas

v=

velocity

xDDT=

DDT distance from spark plug

γ=

ratio of specific heat

Subscript

a=

atmosphere

b=

inside of gas cylinder

c=

combustor

cal=

calculation

d=

detonable mixture

exp=

experiment

f=

fuel

o=

oxidizer

s=

static

steady=

steady flow by cold gas test

t=

total

Acknowledgments

This study was subsidized by Grant-in-Aid for Young Scientists (A) (17H04971), and the Tatematsu Foundation.

Additional information

Funding

This work was supported by the Japan Society for the Promotion of Science Grant-in-Aid for Young Scientists (A) (17H04971); Tatematsu Foundation.

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