A new experimental facility was designed, fabricated, and tested to model and study the effect of bidirectional swirl flow on the rate of heat transfer to combustion chamber walls. Reduction of this heat transfer can result in time and cost of design and fabrication methods of combustion chambers. The experimental study was performed using propane and air with oxygen as fuel and oxidizer, respectively. For similar flow rates, in cases where bidirectional flow was present, wall temperature reductions of up to 70% were observed. In cases where only some of the oxidizer was injected from the chamber end to generate the bidirectional swirl flow, the lowest wall temperature existed. This can be due to better mixing of fuel and oxidizer and absence of hot spots in the combustion core.

1.
Marble
,
F. E.
, 1985, “
Growth of a Diffusion Flame in the Field of a Vortex
,”
Recent Advances in the Aerospace Sciences
, in Honor of Luigi Crocco,
E.
Casci
, ed.,
Plenum
, New York, pp.
395
413
.
2.
Chiaverini
,
M. J.
,
Malecki
,
M. J.
,
Knuth
,
W. K.
, and
Gramer
,
D. J.
, 2003, “
Vortex Thrust Chamber Testing and Analysis for O2-H2 Propulsion Application
,” AIAA Paper No. 2003-4473.
3.
Vyas
,
A. B.
,
Majdalani
,
J.
, and
Chiaverini
,
M. J.
, 2003, “
The Bidirectional Vortex. Part 1: An Exact Inviscid Solution
,” AIAA Paper No. 2003-5052.
4.
Bloor
,
M. I. G.
, and
Ingham
,
D. B.
, 1987, “
The Flow in Industrial Cyclones
,”
J. Fluid Mech.
0022-1120,
178
, pp.
507
519
.
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