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A simple finite-difference technique for the computation of three-dimensional incompressible laminar boundary layers. Part I: Description of the method
A program for the computation of a compressible turbulent boundary layer under infinite swept wing conditions.
Application of Levinsky's method to wings with defelected slipstreams
Behaviour of very large aircraft disturbed by windshear and atmospheric turbulence
Studie van de dynamische eigenschappen van grote vliegtuigen in het bijzonder tijdens nadering en landing: beschouwing van de "handling qualities" en de "side step"-manoeuvre
Flight operational evaluation of approach and runway lighting
Searched for: %2520
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