1–5 von 5 Ergebnissen
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    Shape memory alloy TiNi actuators for twist control of smart wing designs

    Jardine, A.P. / Kudva, J.N. / Martin, C. et al. | Tema Archiv | 1996
    being studied for a subscale model of a fighter aircraft. The use of the SME (Shape Memory Alloy) TiNi for wing twist actuation was investigated ...

    Overview of the DARPA/AFRL/NASA Smart Wing Phase 2 program

    Kudva, J.N. / Sanders, B. / Pinkerton-Florance, J. et al. | Tema Archiv | 2001
    provide variable, optimal aerodynamic shapes for a variety of flight regimes. Two half-span 16% scale wind tunnel models, representative of an ...

    Conformal load-bearing antenna structures (CLAS): initiative for multiple military and commercial applications

    Lockyer, A.J. / Alt, K.H. / Kudva, J.N. et al. | Tema Archiv | 1997
    , fabricate, and test a CLAS component and lay the foundation for future work where potential benefits from structurally integrated antennas may be ...

    Air vehicle integration issues and considerations for CLAS successful. implementation

    Lockyer, A.J. / Alt, K.H. / Kudva, J.N. et al. | Tema Archiv | 2001
    solved for final technology inclusion in an operational air-vehicle. Presented are some key results from the Air Force Research Laboratory's ...

    Adaptive smart wing design for military aircraft: requirements, concepts, and payoffs

    Kudva, J.N. / Appa, K. / Way, C.B. van et al. | Tema Archiv | 1995
    An aircraft adaptive wing can vary its parameters such as camber, and span-wise wing twist canbe varied to optimize the wing shape for ...