Meddelande / Flygtekniska Försöksanstalten, FFA = Report

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Bibliographische Detailangaben
Körperschaft: Flygtekniska Försöksanstalten (VerfasserIn)
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Sprache:swe
Veröffentlicht: Stockholm 1944-
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Monografische Reihe
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Titel Jahr Band
Methods to enhance the accuracy of finite volume schemes II 1991
A solution method for the time-dependent navier-stokes equations for laminar, incompressible flow 1989
Open boundary conditions for the navier-stokes equation 1988
A stability analysis of various patched grid interface conditions for hyperbolic equations 1988
Numerical solution of the euler equations using local grid refinement 1988
The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack 1988
Navier-Stokes Solution for laminar transonic flow over a NACA0012 airfoil 1986
Viscous Flow : Its analysis and computation 1986
Grid generation around car configurations above a flat ground plane using transfinite interpolation 1985
Calculation of transonic flow around two wing-fuselage combinations using a full potential equation method 1983
A fundamental study of the relation between the velocity fields far from upstream of, at and far downstream of a rotor disk in a shear flow 1983
Development of a computer code for a three-dimensional higher order panel method for subsonic potential flow 1983
Measuring the flow properties of slotted testsection walls 1982
A two-dimensional study of the maximum power that can be obtained from a wind turbine in a wind shear layer 1981
The velocity induced by the wake of a wind turbine in a shear layer, including ground effect 1980
A mass-flow probe for measurement in high-enthalpy supersonic boundary layers 1977
Flow disturbances associated with preston tubes in turbulent boundary layers 1977
A combined probe for measurement of mass flow, stagnation temperature, and stagnation pressure in supersonic boundary layers 1977
Buckling of sandwich panels subjected to axial compression, shear forces and lateral pressure 1 Experimental investigation 1977 1
The flow in the boundary layer in the main wing 1977
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