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Aandacht voor veiligheid

Aerts, J. (author), Sprong, T. (author), Bannink, B. (author)

Aandacht voor Veiligheid is een haalbaarheidsstudie waarin wordt verkend welke informatie en methoden beschikbaar zijn om ontwikkelingen op het gebied van waterveiligheid in Nederland op de lange termijn te bestuderen. De studie heeft als opdracht meegekregen om de bandbreedten te verkennen in zowel mogelijke toekomstscenarios als ook de...

report 2008

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Preliminary study of a plug nozzle model in supersonic flow

Bannink, W.J. (author), Houtman, E.M. (author), Schoones, M.M.J. (author)

report 1998

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Experimental and computational study of a blunt cylinder-flare model in high supersonic flow

Houtman, E.M. (author), Bannink, W.J. (author), Timmerman, B.H. (author)

report 1995

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Surface flow visualization of a glancing shock-wave/ boundary-layer interaction

van Oudheusden, B.W. (author), Nebbeling, C. (author), Bannink, W.J. (author)

report 1994

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Flow visualization study of high supersonic flow past a blunt cylinder-cone flare body

Bakker, P.G. (author), Bannink, W.J. (author)

report 1994

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Hypersonic test facility Delft HTF-Delft

Bannink, W.J. (author), Bakker, P.G. (author)

report 1993

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Investigation of the Vortex flow over a sharp-edged delta wing in the transonic speed regime

Bannink, W.J. (author), Houtman, E.M. (author), Ottochian, S.P. (author)

report 1989

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The calibration and measuring procedure of a five-hole hemispherical head probe in compressible flow

Houtman, E.M. (author), Bannink, W.J. (author)

report 1989

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Experimental investigation of the transonic flow at the Leeward side of a delta wing at high incidence

Houtman, E.M. (author), Bannink, W.J. (author)

report 1987

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A curved test section for research on transonic shock wave-boundary layer interaction

Nebbeling, C. (author), Bannink, W.J. (author)

report 1984

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Transonic Mach number determination in a blow-down wind-tunnel with solid walls and a downstream throat

Bannink, W.J. (author), Bakker, P.G. (author)

report 1983

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Numerical solution of transonic normal shock wave-boundary layer interaction using the Bohning-Zierep model

Koren, B. (author), Bannink, W.J. (author)

report 1983

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On the structure of the potential flow field near conical stagnation points in supersonic flow

Bakker, P.G. (author), Bannink, W.J. (author), Reyn, J.W. (author)

report 1980

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Bepaling van het getal van Mach van de transsone stroming in de TST 27 windtunnel met dichte wanden

Bannink, W.J. (author), Bakker, P.G. (author)

report 1979

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On the numerical computation of the supersonic flow field about blunted cones at small angles of incidence

van Dommelen, L.L. (author), Bannink, W.J. (author)

report 1976

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Experimental investigation of the supersonic flow field about a slender cone at high incidences

Nebbeling, C. (author), Bannink, W.J. (author)

report 1976

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Conical stagnation points in the supersonic flow around slender circular cones at incidence

Bakker, P.G. (author), Bannink, W.J. (author)

report 1974

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An experimental investigation of the expansion flow field over a delta wing at supersonic speed

Bannink, W.J. (author), Nebbeling, C. (author)

report 1971

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Enige visuele waarnemingen van de stroming in een twee-dimensionale inlaat met uitwendige compressie, ontworpen voor een getal van Mach van 2,94

Nebbeling, C. (author), Bannink, W.J. (author)

report 1969

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Meting van de specifieke vochtigheid van de lucht in het voorraadvat van de ST15 supersone windtunnel

Nebbeling, C. (author), Bannink, W.J. (author)

report 1969