vliegtuigbouw

' ADAS' structures module: user's maual / F. van Dalen and A. Rothwellschema:ProductModel 'Een terugblik' / J.A. Steketeeschema:ProductModel 3D euler flows around modern airplanes / by J.L. Kuyvenhoven, J.W. Boerstoelschema:ProductModel 40 jaar stabiliteit en besturing van vliegtuigen / O.H. Gerlachschema:ProductModel A calculation method for the viscous flow around multi-component airfoils / by B. Oskamschema:ProductModel A European collaborative investigation of the three-dimensional turbulent shear layers of a swept wing : Garteur AD(AG07) TP048 / by B. van den Bergschema:ProductModel A frequency-domain method for the computation of propeller acoustics / by J.B.H.M. Schultenschema:ProductModel A lifting line model for propeller noise / by H.H. Brouwerschema:ProductModel A measurement system for production flight tests of new aircraft / by R. v.d. Leijgraaf ... [et al.]schema:ProductModel A method for measuring take-off and landing performance of aircraft, using an inertial sensing system / by A. Pool ... [et al.]schema:ProductModel A method of characteristic surfaces : the approximate solution of three-dimensional supersonic flow fields, from the near field up to the sonic boom region / Th.P.M. Hendriksschema:ProductModel A non-gaussian atmospheric turbulence model for flight simulator studies of aircraft handling qualities / by C.J. Jansenschema:ProductModel A numerical comparison between multiple-scales and fem solution for sound propagation in lined flow ducts / by Sjoerd W. Rienstra and Walter Eversmanschema:ProductModel A plane wave synthesis facility for sound transmission measurements on panels / H.M.M. van der Wal and E.A.F.A. Demmenieschema:ProductModel A procedure to apply unsteady transonic viscous corrections in aero-elastic analyses using MSC/NASTRAN / M.S.R. Mangunsongschema:ProductModel A residual correction method applied to 2D multi-point airfoil design and 3D single-point wing design / by Th.E. Labrujère and J. van der Voorenschema:ProductModel A Roe-type scheme for chemically reacting flow in thermal equilibrium / by S.P. Spekreijseschema:ProductModel A simple, robust and fast algorithm to compute deformations of multi-block structured grids / S.P. Spekreijse, B.B. Prananta and J.C. Kokschema:ProductModel A system for transonic wing design with geometric constraints based on an inverse method / by F.J. Brandsma and J.M.J. Frayschema:ProductModel A system look at electromechanical actuation for primary flight control / E.A. Lomonovaschema:ProductModel ... show all 609