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    Rapid Lift-to-Drag Ratio Prediction for NACA Four-Digit Airfoils Using a Deep Neural Network

    Source: Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 001::page 04025106-1
    Author:
    Tekin, Abdurrahman
    ,
    Xiao, Tianhang
    ,
    Yu, Xiongqing
    DOI: 10.1061/JAEEEZ.ASENG-6258
    Publisher: American Society of Civil Engineers
    Abstract: AbstractAirfoil optimization is crucial for enhancing aerodynamic performance and efficiency in aerospace engineering because accurate and rapid predictions of the lift-to-drag ratio (CL/CD) directly influence design decisions. However, traditional methods are ...
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      Rapid Lift-to-Drag Ratio Prediction for NACA Four-Digit Airfoils Using a Deep Neural Network

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4314145
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    contributor authorTekin, Abdurrahman
    contributor authorXiao, Tianhang
    contributor authorYu, Xiongqing
    date accessioned2026-08-20T21:13:37Z
    date available2026-08-20T21:13:37Z
    date copyright2025/09/18
    date issued2026
    identifier otherJAEEEZ.ASENG-6258.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314145
    description abstractAbstractAirfoil optimization is crucial for enhancing aerodynamic performance and efficiency in aerospace engineering because accurate and rapid predictions of the lift-to-drag ratio (CL/CD) directly influence design decisions. However, traditional methods are ...
    publisherAmerican Society of Civil Engineers
    titleRapid Lift-to-Drag Ratio Prediction for NACA Four-Digit Airfoils Using a Deep Neural Network
    typeJournal Article
    journal volume39
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-6258
    journal fristpage04025106-1
    journal lastpage04025106-12
    page12
    treeJournal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 001
    contenttypeFulltext
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