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  • Department of Aircraft Design Engineering
    Department of Aircraft Design Engineering
    Department of Aeronautical Structure Engineering
    Department of Fluid Mechanics
    Department of Integrated Technology and Control Engineering
    Department of Civil Aviation Engineering
    Current Location: English > Departments > Department of Aircraft Design Engineering > Content
    Department of Aircraft Design Engineering
    2012-02-16   審核人:

    The Department of Aircraft Design Engineering was established in October 1952, formerly known as aircraft design faculty working office of the Aircraft Department of HuaDong Aviation College. After merge of the university in October 1957, the department became the aircraft design faculty working office of the Aircraft Department of Northwestern Polytechnical University.

    At present, the department has 33 faculty members, including 8 professors, 12 associate professors. The main research fields of the department is aircraft design, which is the earliest aeronautical field established for country's aviation industry. After 50 years of development, the department continues to meet the needs of the aerospace industry with new concepts, advanced design and its excellent graduates.

    Main research fields

    New concept flight vehicle design

    Configuration design and evaluation technology

    Structural integrated design

    Flight dynamics and control

    Famous professors

     

     

    Professor Gao Zhenghong

    Professor Song Bifeng

     

     

     

    Professor Lv Zhenzhou

    Professor Wang Heping

     

     

     

    Professor Feng Yunwen

     

    Main research results

    1.    New concept flight vehicle design

    Next generation fighter

    Next generation commercial aircraft

    New concept flight vehicles

     

    Adjustable Tail Configuration

     

    Twin-fuselage Configuration

     

    Canard Configuration

     

    Dual-channel Configuration

     

    Joined Wing Configuration

     

    Super-sonic Passenger Airplane

     

    Cycloidal Propelle Vehicles

     

    Micro Flap Wing Air Vehicles

     

    New Concept Compound-Lifting Aircraft

     

    Near Space Airship Design

     

    Aerocar Design

    2.    Configuration design and evaluation technology

    Configuration design

    Combat effectiveness simulation

    Combat survivability analysis and design

     

    Chinese J-7E fighter (double delta wing)

     

    A project of large passage airplane

     

    Collaborative optimization design for C919

     

    Aircraft combat effectiveness analysis and concept assessment/selection system

     

    Aircraft combat survivability analysis and design system

    3.    Structural integrated design

    Structural optimization

    Composite structure analysis and design

    Long-life/high reliability/durability and damage tolerance design

     

    Optimization Design of Wing Structures

     

    Composite Material Tensor Skin Wing

     

    The Fatigue Analysis of Composite Material Flexible-bar Structures

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    Tel: +86-29-88493671
    Email: zheng2014@nwpu.edu.cn
    Copyrights 2019 School of Aeronautics Technical support: Zhao YouGuo
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