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      KCI등재 SCIE SCOPUS

      Multiple Arc Composition Technique for S-Duct Intake Construction Strictly Obeying Area Rule

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      https://www.riss.kr/link?id=A108687650

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      다국어 초록 (Multilingual Abstract)

      A technique was developed to design the intake duct shape by composing multiple arcs to build duct cross-sections, which presents the capability to represent the complex shape of various S-duct intakes by automatically generating intermediate cross-sections between given control cross-sections and flexibility to adjust those cross-sections to strictly obey prescribed area rule. Every cross-section is assumed to have a bilateral symmetric shape. The one half is divided into two pieces, top and bottom, each of which this multi-arc composition technique is applied to build. To overcome the underdetermined system even with the three-arc composition scheme, geometrical parameters are grouped into two sets. One is a set of parameters determined by geometry equations and imposed constraints. The other is a set of parameters obtained by morphing the features of intake cross-sections to fill the gap between the numbers of variables and equations. The concave shape of the intake cross-section can be handled by allowing some geometrical parameters, such as arc radius and angle, to have negative values. Some rules for morphing algorithm and a driving curve in addition to area variation have to be prescribed in advance and they are chosen to change linearly in this study. Demonstrations showed the ability of the three-arc composition technique by successfully generating various S-duct intakes consisting of complex shape cross-sections and strictly obeying a prescribed area rule.
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      A technique was developed to design the intake duct shape by composing multiple arcs to build duct cross-sections, which presents the capability to represent the complex shape of various S-duct intakes by automatically generating intermediate cross-se...

      A technique was developed to design the intake duct shape by composing multiple arcs to build duct cross-sections, which presents the capability to represent the complex shape of various S-duct intakes by automatically generating intermediate cross-sections between given control cross-sections and flexibility to adjust those cross-sections to strictly obey prescribed area rule. Every cross-section is assumed to have a bilateral symmetric shape. The one half is divided into two pieces, top and bottom, each of which this multi-arc composition technique is applied to build. To overcome the underdetermined system even with the three-arc composition scheme, geometrical parameters are grouped into two sets. One is a set of parameters determined by geometry equations and imposed constraints. The other is a set of parameters obtained by morphing the features of intake cross-sections to fill the gap between the numbers of variables and equations. The concave shape of the intake cross-section can be handled by allowing some geometrical parameters, such as arc radius and angle, to have negative values. Some rules for morphing algorithm and a driving curve in addition to area variation have to be prescribed in advance and they are chosen to change linearly in this study. Demonstrations showed the ability of the three-arc composition technique by successfully generating various S-duct intakes consisting of complex shape cross-sections and strictly obeying a prescribed area rule.

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      참고문헌 (Reference)

      1 Haug JP, "Validation of RANS simulations of the flow in a short highly bent intake duct" 2019

      2 Lee BJ, "Optimal shape design of the S-shaped subsonic intake using NURBS" 2005

      3 Lee JG, "Numerical simulation of threedimensional flows for flush inlet" AIAA 2004

      4 Mehdi Miansari ; Sajad Ghezelsofloo ; Davood Toghraie, "Numerical Investigation of Geometrical Design Effect on the Submerged Inlet Aerodynamics Characteristics" 한국항공우주학회 21 (21): 25-38, 2020

      5 Kariminia A, "Full threedimensional inverse design method for S-ducts using a new dimensionless flow parameter" 11 : 1119-, 2021

      6 이지형 ; 이시욱 ; 조진수, "Effect of Inlet Boundary Layer Suction on Flow Distortion in Subsonic Diffusing S-Duct" 한국항공우주학회 20 (20): 850-857, 2019

      7 이유렬 ; 이지원 ; 신창민 ; 명노신, "Double Serpentine 노즐의 단면적과 비행조건 변화에 따른 UCAV의 플룸 유동장 및 IR 특성 연구" 한국항공우주학회 49 (49): 689-698, 2021

      8 Baik YS, "Development of automated cross-section area controlled S-duct modeling technique" 2012

      9 Gan W, "Design optimization of a threedimensional diffusing S-duct using a modified SST turbulent model" 63 : 63-72, 2017

      10 D’Ambros A, "Computational design optimization for S-ducts" 2 : 36-, 2018

      1 Haug JP, "Validation of RANS simulations of the flow in a short highly bent intake duct" 2019

      2 Lee BJ, "Optimal shape design of the S-shaped subsonic intake using NURBS" 2005

      3 Lee JG, "Numerical simulation of threedimensional flows for flush inlet" AIAA 2004

      4 Mehdi Miansari ; Sajad Ghezelsofloo ; Davood Toghraie, "Numerical Investigation of Geometrical Design Effect on the Submerged Inlet Aerodynamics Characteristics" 한국항공우주학회 21 (21): 25-38, 2020

      5 Kariminia A, "Full threedimensional inverse design method for S-ducts using a new dimensionless flow parameter" 11 : 1119-, 2021

      6 이지형 ; 이시욱 ; 조진수, "Effect of Inlet Boundary Layer Suction on Flow Distortion in Subsonic Diffusing S-Duct" 한국항공우주학회 20 (20): 850-857, 2019

      7 이유렬 ; 이지원 ; 신창민 ; 명노신, "Double Serpentine 노즐의 단면적과 비행조건 변화에 따른 UCAV의 플룸 유동장 및 IR 특성 연구" 한국항공우주학회 49 (49): 689-698, 2021

      8 Baik YS, "Development of automated cross-section area controlled S-duct modeling technique" 2012

      9 Gan W, "Design optimization of a threedimensional diffusing S-duct using a modified SST turbulent model" 63 : 63-72, 2017

      10 D’Ambros A, "Computational design optimization for S-ducts" 2 : 36-, 2018

      11 Atasoy M, "Bezier curve-based S-shape optimization for RAE-M2129 inlet" 2019

      12 이영환, "A Numerical Study on Flow-Through Model Design Considering the Internal Loss" 한국항공우주학회 20 (20): 688-696, 2019

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