|Table of Contents|

Effects of airfoil scaling on the predicted aerodynamic performance and forcing of turbine(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2018年06期
Page:
29-38
Research Field:
研究与设计
Publishing date:

Info

Title:
Effects of airfoil scaling on the predicted aerodynamic performance and forcing of turbine
Author(s):
JIANG Jinpeng1 SHI Jingcheng1 SU Lichao1 GONG Fan1 WANG Jue2
1.Science and Technology on Space Physics Laboratory, China Academy of Launch Vehicle Technology, Beijing 100076, China; 2.China Academyof Launch Vehicle Technology, Beijing 100076, China
Keywords:
airfoil scaling numerical simulation aerodynamic performance aerodynamic forcing
PACS:
V434+.11-34
DOI:
-
Abstract:
Effects of vane/blade airfoil scaling on the prediction of aerodynamic performance and unsteady forcing have been investigated for the turbine.A single-stage axial-flow turbine with 18 vanes and 32 blades was adopted.3D steady and unsteady simulations were conducted for configurations with different scaling factors, and the full-scale case was used as the baseline simulation.The results show that the vane/blade airfoil scaling has little influence on the steady and time-averaged pressure on the blade and performance of turbine.The predicted deviation is below 2% even if the scaling deviation exceeds 10%.The fast Fourier transform(FFT)is used to transform the unsteady pressure and forcing predicted in the time domain to obtain the characteristics in the frequency domain.The vane/blade airfoil scaling has little difference on the frequency characteristics of unsteady pressure and aerodynamic forces, while amplitude is greatly affected.The results show that the predicted amplitude deviation is not directly related to the scaling deviation, but the case with small scaling deviation(3.125% in this study)indeed shows relatively stable and minor error.

References:

[1] CIZMAS P G A, DORNEY D J.The influence of clocking on unsteady forces of compressor and turbine blades[J].International journal of turbo jet-engines, 2000, 17: 133-142.
[2] PARK J Y, CHOI M S, BACK J H.Effects of axial gap on unsteady secondary flow in one-stage axial turbine[J].International journal of turbo jet-engines, 2003, 20: 315-333.
[3] CHANG D, TAVOULARIS S.Effect of the axial spacing between vanes and blades on a transonic gas turbine performance and blade loading[J].International journal of turbo jet-engines, 2013, 30(1): 15-31.
[4] TANG E, LEROY G, PHILIT M, et al.Unsteady analysis of inter-rows stator-rotor spacing effects on a transonic, low-aspect ratio turbine [C]//Proceedings of ASME Turbo Expo 2015: Turbine Technical Conference and Exposition.Montréal, Canada, GT2015-42227, 2015
[5] FENG Z P, LI H T, SONG L M, et al.Aerodynamic inverse design optimization for turbine cascades based on control theory[J].Science China technological sciences, 2013, 56(2): 308-323.
[6] 李旭升,郑继坤,吴玉珍.某型超音速冲击式氧涡轮叶型气动优化[J].火箭推进, 2014, 40(5): 44-49.
LI X S, ZHENG J K, WU Y Z.Aerodynamic optimization for blade profile of a supersonic impulse oxygen turbine[J].Journal of rocket propulsion, 2014, 40(5): 44-49.
[7] 郑晓宇,林奇燕,王磊.小型部分进气亚声速涡轮流动损失研究及优化[J].火箭推进, 2017, 43(1): 32-37.
ZHENG X Y, LIN Q Y, WANG L.Research and optimization for flow loss of a small partial admission subsonic turbine[J].Journal of rocket propulsion, 2017, 43(1): 32-37.
[8] KIM J H, CHOI K J, KIM K Y.Aerodynamic analysis and optimization of a transonic axial compressor with casing grooves to improve operating stability[J].Aerospace science and technology, 2013, 29: 81-91
[9] KAWATSU K, TANI N, YAMANISHI N.Numerical study on rotor-stator interaction of a supersonic reaction turbine for a liquid rocket engine[C]//Proceedings of the ASME 2010 3rd Joint US-European Fluids Engineering Summer Meeting and 8th International Conference on Nanochannels, Microchannels, and Minichannels.Montreal, Montreal, Canada, FEDSM-ICNMM2010-30640, 2010.
[10] ZHAO B, YANG C, CHEN S, et al.Unsteadyflow variability driven by rotor-stator interaction at rotor exit[J].Chinese journal of aeronautics, 2012, 25(6): 871-878.
[11] DORNEY D J, GRIFFIN L W, HUBER F, et al.Unsteady flow in a supersonic turbine with variable specific heats[J].Journal of propulsion, 2001, 18(2): 493-496.
[12] DORNEY D J, GRIFFIN L W, HUBER F, et al.Off-design performance of a multi-stage supersonic turbine[C]//41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada, AIAA, 2003
[13] HUDSON S T, ZOLADZ T F, DORNEY D J.Rocket engine turbine blade surface pressure distributions: experiment and computations[J].Journal of propulsion and power, 2003, 19(3): 364-373.
[14] TOKUYAMA Y, FUNAZAKI K, KATO H.Computational analysis of unsteady flow in a partial admission supersonic turbine stage[C]//Proceedings of ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Düsseldorf, Germany, GT2014-26071, 2014
[15] SAKAI N, HARADA T IMAI Y0.Numerical study of partial admission stages in steam turbine[J].JSME international journal series B, 2006, 49(2): 212-217.

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Last Update: 2018-12-25