The influence of a highly integrated flow-through intake on the vortical flow about a generic lambda wing configuration is studied for 0.55·106
Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes
Journal of aircraft ; 52 , 3 ; 972-980
2015
Aufsatz (Zeitschrift)
Englisch
British Library Conference Proceedings | 2012
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