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    • 2022-12Zeitschriftenartikel
      Low speed aerodynamic characteristics of non-slender delta wing at low angles of attack 
      Mohamed, Mohamed Ali; Afgan, Imran; Hefny Salim, Mohamed; Mohamed, Ibrahim K.
      Low-speed wind tunnel experiments are conducted to study the aerodynamic performance of a half-span delta wing with 45° leading-edge sweep at subsonic flow regime. The experiments are carried out at a Reynolds number of ...
      DINI-Zertifikat 2019OpenAIRE validatedORCID Consortium
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