A knowledge-based aerodynamic design method, CDISC, has been leveraged for the computational design exploration of the cruise slotted airfoil as a drag-saving technology for single aisle, transonic transport aircraft. Aerodynamic predictions were generated using the NASA USM3D Reynolds-averaged Navier-Stokes flow solver, and laminar flow assessments were conducted using the NASA BLSTA3D boundary layer profile solver paired with the LASTRAC stability analysis and transition prediction software. The CDISC design method was used to parametrically vary several slotted-airfoil design variables to understand their impact on aerodynamic performance. In addition to establishing best practices for slotted airfoil design, it was observed that the historically noted skin-friction penalty for cruise slotted airfoils was attributed to the low-Reynolds-number boundary layer of the flap. At cruise, this skin-friction penalty negated any potential decrease in pressure drag enabled by the cruise slotted airfoil architecture. This observation led to the development of an Aft-Laminar Multi-element Airfoil concept that uses airfoil shaping to promote natural laminar flow on the flap. At cruise conditions, the concept is predicted to offer a 2.7% reduction in sectional drag relative to a fully turbulent supercritical airfoil. Off-design analyses showed that laminar flow could be maintained with near-cruise variations in angle of attack and Mach number, resulting in sustained aerodynamic efficiency improvements and a delay in the drag rise Mach number. A low-speed, high-lift analysis at takeoff conditions predicted a maximum lift coefficient of 2.4 could be achieved by use of a variable-camber leading edge on the main element and simple deflection of the flap. These computationally-predicted benefits have motivated future research toward an aft-laminar cruise slotted wing design as an incremental step toward the application of natural laminar flow technology on transonic commercial transports.


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    Titel :

    Design Exploration of a Transonic Cruise Slotted Airfoil


    Beteiligte:

    Kongress:

    AIAA Aviation 2021 ; 2021 ; Virtual, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Design Exploration of a Transonic Cruise Slotted Airfoil

    Hiller, Brett R. / Campbell, Richard / Lynde, Michelle N. et al. | AIAA | 2021


    DESIGN EXPLORATION OF A TRANSONIC CRUISE SLOTTED AIRFOIL

    Hiller, Brett R. / Campbell, Richard / Lynde, Michelle N. et al. | TIBKAT | 2021


    Design Exploration of a Transonic Cruise Slotted Airfoil

    Brett Hiller / Richard Campbell / Michelle Lynde et al. | NTRS


    Transonic Cruise Slotted Wing Design for Commercial Transport Aircraft using CDISC

    Hiller, Brett R. / Campbell, Richard L. / Banchy, Michelle N. | AIAA | 2024


    Transonic Cruise Slotted Wing Design for Commercial Transport Aircraft using CDISC

    Brett Hiller / Richard Campbell / Michelle Banchy | NTRS