Combustor exit plane

During the tests, the axial pressure distributions on the upper and lower walls of combustor were measured. In test run No. 2 (see Table 23.1), the total pressure field was measured in the combustor exit plane. Measurements were carried out by a 10-point transversing rake. In the other test runs, the total and static pressures were measured at a single point in the combustor exit plane. 

The boundary condition at impermeable walls and symmetry planes at y and y = a a being the width of the combustor exit) is dp/dy = 0. 

Figure 7. CARS temperature profile of shrouded JT-12 combustor can exhaust 13 cm downstream of exit plane at cruise conditions (13)...

Figure 4. Time-averaged spectrum of N, on exit plane of combustor recorded with collinear beams and without background rejection 10 laser shots are averaged at...

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