1–20 von 40 Ergebnissen
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    Wing-tail interaction flutter revisited

    Yurkovich, R. | Tema Archiv | 1996

    U-groove aluminum weld strength improvement

    Verderaime, V. / Vaughan, R. | Tema Archiv | 1996

    Stress analysis of an orthotropic plate with a plugged center hole

    Hindman, T.W. / Horn, W.J. | Tema Archiv | 1996

    Static test induced loads verification beyond elastic limit

    Verderaime, V. / Harrington, F. | Tema Archiv | 1996

    Semiactive vibration suppression of truss structures by ER fluid damper

    Onoda, J. / Oh, H.U. / Minesugi, K. | Tema Archiv | 1996

    Recent enhancements to PANDA2

    Bushnell, D. | Tema Archiv | 1996

    Random parametric vibration in aircraft landing gear

    Huntington, D.E. / Lyrintzis, C.S. | Tema Archiv | 1996

    Optimization of analysis methods for space shuttle orbiter RCC hardware

    Chi, C.T. / Okino, D. / McCleary, B. | Tema Archiv | 1996

    On the use of component modes in multibody dynamics

    Craig, R.R. jun. / Anthony, T.C. | Tema Archiv | 1996

    Nonlinear analysis of the space shuttle super-lightweight external fuel tank

    Nemeth, M.P. / Britt, V.O. / Collins, T.J. et al. | Tema Archiv | 1996

    Integration of a generic flight control system into ASTROS

    Volk, J. / Ausman, J.D. | Tema Archiv | 1996

    Inclusion of transverse shear deformation in optimum design of aircraft wing panels

    Williams, P.W.L. / Williams, F.W. / Kennedy, D. | Tema Archiv | 1996