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논문 기본 정보

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학위논문
저자정보

김준희 (인하대학교, 인하대학교 대학원)

지도교수
김광용
발행연도
2019
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이 논문의 연구 히스토리 (9)

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In order to improve the engine power and thermal efficiency, modern gas turbines employ various cooling techniques for turbine blades. Film cooling is a most popular external cooling technique, which uses discrete holes located on external surface of a turbine blade to eject coolant air to generate a coolant layer between the blade surface and hot gas. The present study proposes novel film-cooling holes with converged inlet shape, and investigated the influence of the inlet shape on film-cooling performance. In addition, a bended hole was numerically formulated and optimized using surrogate-based optimization techniques. Three-dimensional numerical analyses for fluid flow and heat transfer were performed based on Reynolds-averaged Navier-Stokes equations for the inlet shaped holes.
First, a bended hole was studied to evaluate the effects of geometric variables on the film-cooling performance, and optimized. The spatially-averaged film-cooling effectiveness was employed as the objective function, and the injection angles of the lower and upper cylindrical parts and height of the bending point were selected as design variables for optimization The Kriging model was used to approximate the objective function. 27 design points were selected by the Latin hypercube sampling, where objective function values were calculated to construct the surrogate model, i.e., Kriging model. The results showed that the optimum bended film-cooling hole improved the spatially-averaged film-cooling effectiveness compared to a reference bended hole and a cylindrical hole.
Second, a converged-inlet shape for cylindrical film-cooling holes is proposed. A parametric study was performed for the converged-inlet shaped hole with four geometric parameters: the streamwise and lateral expansion angles, injection angle, and the ratio of the length to the diameter of the cylindrical part of the holes. The computational results showed that the converged-inlet shaped hole resulted in about 46.5% improvement of the spatially film-cooling effectiveness compared to a cylindrical film-cooling hole. The film-cooling performance was sensitive to all four geometric parameters.
Finally, a converging-diverging film-cooling hole was designed by combining a converged inlet with a fan-shaped exit. The performance of the proposed design was compared to that of a fan-shaped hole. Compared to the fan-shaped hole, the converging-diverging hole improved the spatially averaged film-cooling effectiveness by 4.34%, 5.91%, and 9.88% at blowing ratios of 0.5, 1.0, and 1.5, respectively. These improved film-cooling performances were achieved by reducing the size of the separation bubble in the hole, thus increasing the thickness of the coolant layer downstream of the hole.

목차

ABSTRACT ··········································································I
TABLE OF CONTENTS ·························································III
NOMENCLATURE ······························································V
TABLE CAPTIONS ·····························································VII
FIGURE CAPTIONS ···························································VIII
1. INTRODUCTION ·······························································1
1.1 Background ····································································1
1.2 Literature Survey ······························································4
1.2.1 Cylindrical film-cooling hole·······································4
1.2.2 Shaped film-cooling hole ···········································5
1.3 Motivations and Objectives ················································8
2. NUMERICAL ANALYSIS ····················································10
2.1 Configuration of the film-cooling holes ··································10
2.2 Computational Domain, Grid, and Boundary Conditions ··············11
2.3 Reynolds-Averaged Navier Stokes Equations ···························15
2.4 Shear Stress Transport Turbulence Model ·······························17
2.5 Convergence Criteria ························································19
3. OPTIMIZATION NETHODOLOGY ······································20
3.1 Design Space ·································································20
3.2 Design of Experiments ······················································20
3.3 Kriging Model ·······························································21
3.4 Single-Objective Optimization ············································22
4. RESULTS AND DISCUSSION ··············································24
4.1 Performance Index ··························································24
4.2 Grid Dependency Test ······················································26
4.3 Validation of CFD Results ··················································28
4.3.1 Bended hole and converged inlet hole ···························28
4.3.2 Converging-diverging film-cooling hole ························28
4.4 Optimization of Bended Film Cooling Hole ·····························31
4.4.1 Objective function and design variables ························31
4.4.2 Parametric study ····················································32
4.4.3 Optimization results ················································34
4.5 Performance evaluation of a converged inlet shaped hole ·············48
4.5.1 Geometric parameters and performance function ··············48
4.5.2 Comparative study ·················································51
4.5.3 Parametric Study ···················································57
4.6 Performance evaluation of a converging diverging hole ·············72
4.6.1 Configuration of proposed converging-diverging hole ········72
4.6.2 Comparative study ·················································75
5. CONCLUSIONS ·······························································87
5.1 Concluding Remarks ························································87
5.2 Future works ·································································89
REFERENCES ·····································································90
AUTHOR’S PUBLICATIONS ··················································96

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