Space mining; is the universe up for grabs?

A two-parameter method for eN transition prediction

A correction to the eN method for transition prediction, that at present is in use at Delft University, is developed and tested. The existing method is based on solutions of the Falkner-Skan similar boundary layer equation without suction or blowing. The correction is based on additional solutions of this equation with suction and blowing. For...

The eN method for transition prediction: Historical review of work at TU Delft

Overview of stability and transition in external aerodynamics

The boundary layer along the fuselage, wings and tailplanes of aircraft will usually be laminar at the leading edge and will become unstable further downstream. Once the boundary layer has become unstable it will undergo transition to turbulence. Stability and transition can be considered as one of the most complex problems of fluid dynamics....

VTH - LR - Delft aerospace een halve eeuw in stroming en sturing

Essays on aerodynamics: A collection of scientific papers and some personal impressions dedicated to Professor J.A. Steketee

Bereiding van aceton volgens het Wacker-procede

Document uit de collectie Chemische Procestechnologie

Theorie en experiment in de stromingsleer

De ontwikkeling van vleugelprofielen

Theoretical and experimental investigations of incompressible laminar boundary layers with and without suction

Reisverslag: AGARD - Wind tunnel and model testing panel boundary layer research meeting Londen, Engeland, 25 tm. 29 april 1960

Verslag van een bezoek door Prof.dr.ir. H.J. van der Maas en ir. J.L. van Ingen gebracht aan het Engineering Laboratory van de Universiteit van Cambridge vanaf 30 april tot 2 mei 1959