1–5 von 5 Ergebnissen
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    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 ...

    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 ...

    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 ...

    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 ...

    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 ...