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Tests on the afwal 65° Delta wing at NLR: A study of vortex flow development between Mach =0,4 and 4Boersen, S.J. (author), Elsenaar, A. (author)As part of the US/European Vortex Flow Experiment force and pressure measurements have been carried out in the transonic and supersonic wind tunnels of NLR on a 65° swept delta wing configuration. The larger part of the experimental results concerns a configuration with a sharp and one with a rounded leading edge, both tested over a range of...report 1986
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Boersen, S.J. (author), Elsenaar, A. (author)An evaluation is presented of the half-model test technique based on a systematic comparison of halfmodel test results with the corresponding full-model data. It is shown that the most important problems with this technique originate from half-model mounting and wall interference effects. At present, these effects can only be determined...report 1983