비행 공기역학 해석 연구 환경
비행 공기역학 해석 문제를 사이버인프라스트럭처 환경에서 수행하고 논의하는 사이트
SERVICES
비행 공기 역학 해석 특화 사이트에서는 다음과 같은 유동해석 연구환경을 제공합니다.
비행 공기 역학 해석 시뮬레이션
날개 공력해석에서 정확도가 검증된 비행 공기 역학 해석 시뮬레이션 소프트웨어를 멀티코어로 활용할 수 있습니다.
해석 프로젝트
자신만의 프로젝트를 생성하고 프로젝트 기반에서 시뮬레이션 수행, Airfoil 데이터 분석 등이 가능합니다.
데이터셋 추론
자신이 수행한 해석 데이터 등의 저장소를 활용하고 다양한 데이터들을 서로 공유하고 조회 할 수 있는 페이지를 제공합니다.
관련 문헌
비행공기역학 분야의 논문, 강의자료 등을 확인하실 수 있습니다.
Publications
Papers, Documents, Slide materials, and etc.
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Internationals Journals
A New Crossflow Transition Onset Criterion for RANS Turbulence Models link
Application of Crossflow Transition Criteria to Local Correlation-Based Transition Model link
Correlation-Based Transition Transport Modeling for Three-Dimensional Aerodynamic Configurations link
DLR Contribution to the First High Lift Prediction Workshop link
EUROLIFT Test Case Description for the 2nd High Lift Prediction Workshop link
Finite Element Flow Simulations of the EUROLIFT DLR-F11 High Lift Configuration link
FUN3D and CFL3D Computations for the First High Lift Prediction Workshop link
Grid-Adapted FUN3D Computations for the Second High Lift Prediction Workshop (Invited) link
High Lift OVERFLOW Analysis of the DLR F11 Wind Tunnel Model link
Overview and Summary of the Second AIAA High Lift PredictionWorkshop (Invited) link
A comprehensive study of detached-eddy simulation link
A hybrid RANS-LES approach with delayed-DES and wall-modelled LES capabilities link
Adaptation of Eddy-Viscosity Turbulence Models to Unsteady Separated Flow Behind Vehicles link
Comments on the Feasibility of LES for Wings, and on a Hybrid RANS LES Approach link
Detached Eddy Simulation of Flow around A-Airfoil link
Detached Eddy Simulations of Hypersonic Transition link
Detached-Eddy Simulation of the vortical flow field about the VFE-2 delta wing link
Detached-Eddy Simulations of Attached and Detached Boundary Layers link
Guidelines for implementing Detached-Eddy Simulation using different models, Anwendung unterschiedlicher Modelle bei der Detached-Eddy Simulation link
Hybrid LES-RANS modelling - a one-equation SGS model combined with a k–w model for predicting recirculating flows link
Implementation of preconditioned dual-time procedures in OVERFLOW link
Improvement of delayed detached-eddy simulation for LES with wall modelling link
Numerical assessment of turbulent models at a critical regime on unstructured meshes link
trends and challenges in modelling complex turbulent flows link
Validation of DES-SST Based Turbulence Model for a Fully Developed Turbulent Channel Flow Problem link
Assessment of CFD CSD coupled aeroelastic analysis solution for HART II rotor incorporating fuselage effects link
Correlation of Aeroelastic Response and Structural Loads for a Rotor in Descent link
Delayed detached-eddy simulation of vortex breakdown over a 70° delta wing link
Development and Application of Improved Transition Model Based on Local Correlation-based Transition Model link
Extensive Validation of CFD CSD Aeroelastic Simulations for a Helicopter in Descending Flight link
KFLOW Results of Airloads on HART-II Rotor Blades with Prescribed Blade Deformation link
Low-Reynolds number flow computation for eppler 387 wing using hybrid DES transition model link
Modeling and Prediction of the Crossflow Transition Using Transition Transport Equations link
Validation of HART II Structural Dynamics Predictions Based on Prescribed Airloads link
Numerical simulation study on transitional flow over the KARI-11-180 airfoil using γ-Re Ɵ transition model link
Automatic Transition Prediction and Application to Three-Dimensional Wing Configurations link
eN transition prediction for 3D wing configurations using database methods and a local, linear stability code link
Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code link
Numerical Aspects of Transition Prediction for Three-Dimensional Configurations link
Transition Modeling in FLOWer — Transition Prescription and Prediction link
Transition Prediction for Three-Dimensional Configurations link
Transition prediction for three-dimensional flows using parallel computation link
Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes link
Transition Modeling for General CFD Applications in Aeronautics link
Transition Modelling for General Purpose CFD Codes link
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Technical Reports
PreFLOW User Manual link
KFLOW User Manual link
(TR-AVT-080-TOC)Vortex Breakdown over Slender Delta Wings link
(TR-AVT-080-01)Chapter 1 – INTRODUCTION AND HIGHLIGHTS link
(TR-AVT-080-06)Chapter 6 – UNSTEADY ASPECTS OF LEADING-EDGE VORTICES link
(TR-AVT-080-13)Chapter 13 – UNSTEADY EULER AND DETACHED-EDDY SIMULATIONS OF FULL-SPAN ONERA 70° DELTA WING link
(TR-AVT-080-14)Chapter 14 – GRID STUDY FOR EULER SIMULATIONS OF A 70° DELTA WING WITH THE UNSTRUCTURED FLOW SOLVER EDGE link
(TR-AVT-080-15)Chapter 15 – HIGH REYNOLDS NUMBER DETACHED-EDDY SIMULATIONS OF VORTEX BREAKDOWN OVER A 70 DEGREE DELTA WING link
(TR-AVT-080-16)Chapter 16 – RANS SOLUTIONS OF 70° DELTA WING IN STEADY FLOW link
(TR-AVT-080-17)Chapter 17 – STEADY RANS SIMULATIONS OF A 70° DELTA WING – WITH TUNNEL EFFECTS link
(TR-AVT-080-18)Chapter 18 – SIMULATION OF VORTICAL FLOW OVER ONERA 70-DEGREE DELTA WING EXPERIENCING VORTEX BREAKDOWN link
(TR-AVT-113-20)Chapter 20 – EXPERIMENTAL INVESTIGATIONS ON THE VFE-2 CONFIGURATION AT ONERA, FRANCE link
(TR-AVT-113-26)Chapter 26 – NUMERICAL SOLUTIONS FOR THE VFE-2 CONFIGURATION ON STRUCTURED GRIDS AT ONERA, FRANCE link
(TR-AVT-113-29)Chapter 29 – SHOCK EFFECTS ON DELTA WING VORTEX BREAKDOWN link
3D CFD computations of transitional flows using DES and a correlation based transition model link
2D and 3D Numerical Investigation of the Laminar and Turbulent Flow Over Different Airfoils Using OpenFOAM link
Detached-Eddy Simulation link
Turbulence Modeling for Engineering Flows link
