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Van Ingen, J. (author)
journal article 2012
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Van Ingen, J.L. (author), Kotsonis, M. (author)
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...
conference paper 2011
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Van Ingen, J.L. (author)
conference paper 2008
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Henkes, R.A.W.M. (author), Van Ingen, J.L. (author)
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....
book 1998
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Van Ingen, J.L. (author)
public lecture 1997
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Bakker, P.G. (author), Coene, R. (author), Van Ingen, J.L. (author)
book 1992
document
Van Ingen, H.W.T.J. (author)
Document uit de collectie Chemische Procestechnologie
report 1979
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Van Ingen, J.L. (author)
public lecture 1971
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Van Ingen, J.L. (author)
public lecture 1968
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Van Ingen, J.L. (author)
doctoral thesis 1965
document
Van Ingen, J.L. (author), Tennekes, H. (author)
report 1960
document
Van Ingen, J.L. (author)
report 1959
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