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    Real-Time Transient Three Spool Turbofan Engine Simulation: A Hybrid Approach 

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 005:;page 51602
    Author(s): Naveed U. Rahman; James F. Whidborne
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a transient three-spool turbofan engine simulation model that uses a combination of intercomponent volume and iterative techniques. The engine model runs in real time and has ...
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    Identification of Nonlinearity Sources in a Flexible Wing 

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005:;page 04025060-1
    Author(s): Gabriele Dessena; Alessandro Pontillo; Dmitry I. Ignatyev; James F. Whidborne; Luca Zanotti Fragonara
    Publisher: American Society of Civil Engineers
    Abstract: High aspect ratio flexible wings are of increasing interest for enhancing the aerodynamic efficiency of future designs. However, they often exhibit nonlinear dynamic behavior, complicating both testing and analysis. This ...
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    Degraded Planary Tracking Control of an Omnidirectional Vectored-Thruster Aerostat 

    Source: Journal of Aerospace Engineering:;2019:;Volume (032):;issue:004
    Author(s): Li Chen;James F. Whidborne;Qi Dong;Dengping Duan;Jinguo Liu
    Publisher: American Society of Civil Engineers
    Abstract: The problem of horizontal-plane tracking control of an omnidirectional, four vectored-thruster aerostat subjected to actuator failure is considered. The actuator failures result in the aerostat’s becoming underactuated, ...
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    Degraded Planary Tracking Control of an Omnidirectional Vectored-Thruster Aerostat 

    Source: Journal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 004
    Author(s): Li Chen; James F. Whidborne; Qi Dong; Dengping Duan; Jinguo Liu
    Publisher: American Society of Civil Engineers
    Abstract: The problem of horizontal-plane tracking control of an omnidirectional, four vectored-thruster aerostat subjected to actuator failure is considered. The actuator failures result in the aerostat’s becoming underactuated, ...
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    Active Stall Flutter Suppression for a Revised Leishman–Beddoes Model 

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 001:;page 04023101-1
    Author(s): Junruoyu Zheng; Alessandro Pontillo; Lejun Chen; James F. Whidborne
    Publisher: ASCE
    Abstract: This paper proposes a nonlinear disturbance observer (NDO)–based sliding mode control (SMC) method to the problem of stall flutter suppression for a revised Leishman–Beddoes (L–B) model. To capture accurate aerodynamic ...
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