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Zandbergen, B.T.C. (author)Typical Solid Propellant Rocket Motors (shortly referred to as Solid Rocket Motors; SRM's) are described with the purpose to form a database, which allows for comparative analysis and applications in practical SRM engineering.report 2013
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- Stok, B.P.E. (author), Tuink, S. (author), Zandbergen, M.W. (author) report 2002
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- Zandbergen, B.T.C. (author) report 1995
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- Maree, A.G.M. (author), Mooij, E. (author), Zandbergen, B.T.C. (author) report 1994
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- Mooij, E. (author), Maree, A.G.M. (author), Zandbergen, B.T.C. (author) report 1993
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- Zandbergen, B.T.C. (author) report 1992
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- Wittenberg, H. (author), Korting, P.A.O.G. (author), Zandbergen, B.T.C. (author), Wijchers, T. (author), Elands, P.J.M. (author), de Wilde, J.P. (author), Dijkstra, F. (author) report 1990
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- Wittenberg, H. (author), Korting, P.A.O.G. (author), Zandbergen, B.T.C. (author), Wijchers, T. (author), Elands, P.J.M. (author), de Wilde, J.P. (author), Dijkstra, F. (author) report 1990
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- Wittenberg, H. (author), Korting, P.A.O.G. (author), Zandbergen, B.T.C. (author), Wijchers, T. (author), Elands, P.J.M. (author), de Wilde, J.P. (author), Dijkstra, F. (author) report 1989
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- Wittenberg, H. (author), Korting, P.A.O.G. (author), Zandbergen, B.T.C. (author), Wijchers, T. (author), Elands, P.J.M. (author), de Wilde, J.P. (author), Dijkstra, F. (author) report 1989
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- Wittenberg, H. (author), Korting, P.A.O.G. (author), Zandbergen, B.T.C. (author), Wijchers, T. (author), Elands, P.J.M. (author), de Wilde, J.P. (author), Dijkstra, F. (author) report 1988
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- Wittenberg, H. (author), Korting, P.A.O.G. (author), Zandbergen, B.T.C. (author), Wijchers, T. (author), Elands, P.J.M. (author), de Wilde, J.P. (author), Dijkstra, F. (author) report 1988
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Zandbergen, T. (author)An experimental investigation was carried out in the low speed wind tunnel LST to study aircraft engine noise generation by rotor/stator interaction. Reported is a follow-up experiment including detailed acoustic measurements in the duct downstream of a rotor with cylindrical pins to complement earlier tests whereby rotor wake velocities and...report 1987
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Zandbergen, T. (author)An experimental investigation was carried out to study aircraft engine noise generation by rotor/stator interaction. The experiment was designed to enable a first step verification of a theoretical fan noise model and to indicate further developments which may be needed to provide a representative acoustic field modelling for engine duct liner...report 1987
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- Zandbergen, T. (author) report 1984
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Zandbergen, T. (author), Sarin, S.L. (author), Donnelly, R.P. (author)Results of sound pressure measurements on the fuselage wall of a twin engine propeller driven model are presented. The tests were carried out in the German-Dutch low speed wind tunnel DNW in the Netherlands. The model was equipped with either metallic propeller blades or composite blades. The propeller diameter was 0.762 m. Six microphones were...report 1984
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- Zandbergen, T. (author), de Wolf, W.B. (author), Schulten, J.B.H.M. (author) report 1983
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Zandbergen, T. (author), Sarin, S.L. (author), Laan, J.N. (author), Zeemans, H.J. (author)Acoustic measurements were carried out in the engine intake ducts of a Fokker F28 aircraft during flight. One of the two tail-mounted, low by-pass ratio engines having a hard-walled intake was instrumented to determine the amplitudes of the circumferential modes which constitute the sound field. In the other engine the impedance of the inlet...report 1983
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Zandbergen, T. (author)A three-microphone technique is presented for in-situ acoustic impedance measurements on double layer liners of the Helmholtz resonator type. It can be used under conditions of flow and arbitrary noise sources. The emphasis of this paper is the practical application of this technique, including microphone installation and the implications of...report 1981
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Zandbergen, T. (author), Martlew, D.L. (author)The National Aerospace Laboratory NLR in the Netherlands and the National Gas Turbine Establishment NOTE operate similar acoustic flow duct facilities but with differences in their respective approaches to the measurement of attenuation and impedance of duct linings. A joint exercise was arranged with the object of comparing methods and results,...report 1981
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