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A wind-tunnel investigation was carried out on an oscillating model of the F-5 wing with and without an external store (AIM-9J missile). Detailed steady and unsteady pressure distributions were obtained over the wing, while on the store total aerodyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::85c38f72433d1a639329f25a2dc20492
https://doi.org/10.21236/ada077370
https://doi.org/10.21236/ada077370
