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Licensed Unlicensed Requires Authentication Published by De Gruyter September 18, 2020

Combined Flow Control of Positively Bowed Blade and Vortex Generator Jet on a Compressor Cascade

  • Longting Li EMAIL logo , Yanping Song and Fu Chen

Abstract

A combined flow control method based on positively bowed blade and endwall vortex generator jet (VGJ) was performed to a compressor cascade under three kinds of inlet conditions. The results show that the endwall VGJ can further decrease the total losses in positively bowed cascades. At 0° incidence with zero inlet boundary layer, the separation type in the positively bowed blade is open, with the VGJ, the loss reduction is 2.7 %. As the inlet boundary layer thickens at 0° incidence, the separation region increases with the separation type keeping unchanged, the loss reduction increasing to 11.73 %. As the incidence rises to +7° with zero inlet boundary layer, the separation type converts into closed and the flow separation is the severest in the three cases, with the VGJ, however, the loss reduction is just 7.4 %, which means that the control effect of endwall VGJ not only depends on the size of separation region but also relies on the type of separation mode. If the separation type is open, as the size of separation region expands, the control effectiveness of endwall VGJ increases; if the separation type converts into closed with the further aggravation of flow field, that control effect will decrease.

PACS: (47.32)

Funding statement: This work was supported by the “National Natural Science Foundation of China” (Grant No. 50976026) and “Research Groups of the National Natural Science Foundation of China” (Grant No. 51121004).

Nomenclature

h

blade height, mm

t

pitch, mm

Cax

axial chord length, mm

Lx

axial distance from the jet hole to the leading edge, mm

Ly

circumferential distance from the jet hole to the leading edge, mm

α

pitch angle, °

δ

skew angle, °

y+

wall function

m˙

mass flow rate, kg /s

p*

total pressure, Pa

p

static pressure, Pa

ω

total pressure loss coefficient

U

velocity

S

saddle point

F

spiral point

N

nodal point

BL

boundary layer

PBD

positively bowed blade

VGJ

vortex generator jet

Subscripts
1

cascade inlet

2

cascade outlet

jet

jet tube inlet

m

main flow

e

endwall

0

without flow control

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Received: 2017-03-27
Accepted: 2017-05-07
Published Online: 2020-09-18
Published in Print: 2020-09-25

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