vliegeigenschappen

A break-down of sting interference effects / by A. Elsenaar and S.O.T.H. Hanschema:ProductModel A comparative evaluation of three take-off performance monitor display types / by J.J.L.H. Verspray and R. Khatwaschema:ProductModel A pilot model for helicopter manoeuvres / J. van der Vorstschema:ProductModel A robust quasi-simultaneous interaction method for a full potential flow with a boundary layer with application to wing/body configurations : (Progress report) / by A.J. van der Wees and J. van Muijdenschema:ProductModel A survey on Schiphol Airport of the contamination of wing leading edges of three different aircraft types under operating conditions / by A. Elsenaar and H.N. Haasnootschema:ProductModel Accurate and efficient vortex-capturing for rotor a helicopter rotor in hover / O.J. Boelens ... [et al.]schema:ProductModel Accurate and efficient vortex-capturing for rotor blade vortex interaction / O.J. Boelens ... [et al.]schema:ProductModel Acquiring tail load spectra from in-flight measurements / by P.A. van Gelderschema:ProductModel Advanced propeller performance calculation by a lifting surface method / by J.B.H.M. Schultenschema:ProductModel Aircraft manoeuvring aerodynamics with an unsteady, higher-order panel method, theory and application / E.A.C. Weberschema:ProductModel Aircraft performance data in the aircraft industry / author: H. Wittenbergschema:ProductModel An accurate and robust algorithm for the in-sphere criterion for automated Delaunaybased tetrahedral grid generation / J.W. van der Burgschema:ProductModel An experimental study of the flow over a sharp-edged delta wing at subsonic and transonic speeds / by A. Elsenaar and H.W.M. Hoeijmakersschema:ProductModel Analyses of aircraft responses to atmospheric turbulence / Willem Hendrik Jan Joseph van Staverenschema:ProductModel Analysis of computational aeroelastic simulations by fitting time signals / by M.H.L. Hounjet, B.J.G. Eussen and M.W. Soijerschema:ProductModel Angle-of-attack vane calibration in non-stationary flight : flight test results for the 1998 Cessna Citation II angle-of-attack vane calibration / M.W. Soijerschema:ProductModel Application of aeroelastic methods to predict flutter characteristics of fighter aircraft in the transonic speed range / by J.J. Meijerschema:ProductModel Application of an euler-equation method to a sharp-edged delta-wing configuration with vortex flow / by H.W.M. Hoeijmakers and J.I. van den Bergschema:ProductModel Beyond the frequency limits of time-linearized methods / by M.H.L. Hounjet and B.J.G. Eussenschema:ProductModel Calculation methods for the performance certification of the Euro-Enaer Eaglet / Arjan Poelsschema:ProductModel ... show all 69