An experimental and computational study of the ramped bleed slot in a compressor cascade is presented. The geometry is a circumferential slot downstream of the stator blade trailing edge, with endwall ramps inside the blade passage, and the paper builds on work previously reported for different bleed off-take geometries (Leishman et al., 2007, ASME J. Turbomach., 129, pp. 645–658; Leishman et al., 2007, ASME J. Turbomach., 129, pp. 659–668). The strong interaction between any bleed slot and the primary flow through the cascade can be strong, thereby causing the levels of loss and blockage in the primary flow leaving the blade passage to be increased at some bleed flow rates. Radial flow into the bleed slot is highly nonuniform because the blade-to-blade pressure field causes flow to enter the bleed slot preferentially where the static pressure is high, and to spill out into the primary flow where the static pressure is low. The mechanism for the ramped bleed slot is different from that described in the earlier papers for other geometries. For the ramped bleed slot a static pressure field, with large variations of static pressure in the circumferential direction, is set up in the slot because the endwall flow entering the slot has higher stagnation pressure downstream of the pressure surface than downstream of the suction surface of the upstream blades. The flow entering the slot with high stagnation pressure is brought to rest in a stagnation point on the downstream surface of the slot, and the consequent variation in static pressure on the rear surface sets tangential and radial components of velocity which are a large fraction of the freestream velocity. As well as demonstrating the mechanism for the flow behavior, the paper presents results of experiments and calculations to demonstrate the behavior and gives guidance for the design of bleed slots by stressing the fundamental features of the flow.
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October 2007
Research Papers
Mechanism of the Interaction of a Ramped Bleed Slot With the Primary Flow
B. A. Leishman,
B. A. Leishman
Rolls-Royce plc.
, Derby DE24 8BJ, UK
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N. A. Cumpsty
N. A. Cumpsty
Rolls-Royce plc.
, Derby DE24 8BJ, UK
Search for other works by this author on:
B. A. Leishman
Rolls-Royce plc.
, Derby DE24 8BJ, UK
N. A. Cumpsty
Rolls-Royce plc.
, Derby DE24 8BJ, UKJ. Turbomach. Oct 2007, 129(4): 669-678 (10 pages)
Published Online: December 21, 2006
Article history
Received:
December 7, 2006
Revised:
December 21, 2006
Connected Content
This is a correction to:
Effects of Bleed Rate and Endwall Location on the Aerodynamic Behavior of a Circular Hole Bleed Off-Take
A correction has been published:
Effects of Inlet Ramp Surfaces on the Aerodynamic Behavior of Bleed Hole and Bleed Slot Off-Take Configurations
Citation
Leishman, B. A., and Cumpsty, N. A. (December 21, 2006). "Mechanism of the Interaction of a Ramped Bleed Slot With the Primary Flow." ASME. J. Turbomach. October 2007; 129(4): 669–678. https://doi.org/10.1115/1.2752193
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