WH
W.F. Holtslag
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The Steady Laminar Flamelet Combustion Model was used in combination with the Improved Delayed Detached Eddy turbulence model. A model rocket combustor was simulated with these models. Combustion was performed with gaseous methane and oxygen, injected non-premixed. Experimental data was available for the pressure and wal heat flux to validate the simulation model.
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The Steady Laminar Flamelet Combustion Model was used in combination with the Improved Delayed Detached Eddy turbulence model. A model rocket combustor was simulated with these models. Combustion was performed with gaseous methane and oxygen, injected non-premixed. Experimental data was available for the pressure and wal heat flux to validate the simulation model.
Advanced Hovering Emergency Aid Delivery (AHEAD)
A sustainable unmanned VTOL cargo delivery system
Bachelor thesis
(2015)
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Bart Alewijnse, Jasper Caron, Edvinas Gelezinis, W.F. Holtslag, A. Kenger, D.J. Mansvelder, R. Reiff, S.J. de Roos, Charlotte Schubert, Casper Voogt, R.N.H.W. van Gent, V.P. Brügemann, S.F. Armanini