Based on logged measurements with our very early DS-51-FAN 3-ph during the flight and theoretical background as well as wind tunnel measurements on our DS-51-DIA 3-ph we now would like to describe an approach for the configuration of intake and outlet ducts. The most outstanding characteristic when designing the ducting is a reasonable distribution of the cross-sectional …
After mathematically ensuring the performance of the jet the next step should be to control the stall speed in order to avoid surprises at the take off and landing phase.A usual criterion for estimating smooth and trouble-free handling of the model on normal airfields is the well-established method of measuring the wing loading. This is …
Case Study: Minijets Stinger with DS-51-AXI HDS and HET 700-68-1125kV In order to avoid a disappointment due to unexpected flight behaviour or insufficient performance of the planned model, we would like to take the opportunity to present some substantiated criteria enabling the realisation of the favoured characteristics for the model. A simple calculator is sufficient …
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