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Publikováno v:
Applied Mechanics and Materials. :4156-4160
This paper describes the wind tunnel testing of a Blended Wing Body (BWB) with rectangular canards and twisted wing (Baseline II E2 configuration) developed in Universiti Teknologi MARA (UiTM). The experiment work was carried out in UiTM low speed wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e44bc01fc3b7d4a3cbdf37a8034b437
https://doi.org/10.4028/www.scientific.net/amm.110-116.4156
https://doi.org/10.4028/www.scientific.net/amm.110-116.4156
