{"id":2332972625,"date":"2026-01-07T22:51:03","date_gmt":"2026-01-07T22:51:03","guid":{"rendered":"https:\/\/wwww.tespam.org\/cfd-analysis-of-lift-drag-and-moment-coefficients-of-a-tandem-airfoil-under-ground-effect\/?p=2332972625"},"modified":"2026-08-07T22:14:36","modified_gmt":"2026-08-07T19:14:36","slug":"cfd-analysis-of-lift-drag-and-moment-coefficients-of-a-tandem-airfoil-under-ground-effect","status":"publish","type":"post","link":"https:\/\/www.tespam.org\/wordpress\/cfd-analysis-of-lift-drag-and-moment-coefficients-of-a-tandem-airfoil-under-ground-effect\/","title":{"rendered":"CFD analysis of lift, drag, and moment coefficients of a tandem airfoil under ground effect"},"content":{"rendered":"

Yazar(lar):<\/strong> Mehmet Bak\u0131rc\u0131<\/p>\n

\u00d6zet:<\/strong>
In the present study, an examination of the aerodynamic characteristics in tandem airfoil systems experiencing ground effect was performed. The research was carried out using Computational Fluid Dynamics (CFD) analyses. The effects of multiple parameters, such as angle of attack (AOA) at 0\u00b0, 4\u00b0, and 8\u00b0, horizontal distance between the front and rear airfoils (d\/c), proximity to the ground (h\/c) and Reynolds number on lift (CL), drag (CD), and moment (Cm) coefficients were investigated. The best aerodynamic performance (maximum CL\/CD) was achieved at a 4\u00b0 AOA, very close to the ground (h\/c=0.1), in the range of 1\u2264d\/c\u22642 and higher Reynolds number. It was also determined that the 0\u00b0 AOA exhibited a distinctly different behavior from the other angles (4\u00b0 and 8\u00b0), as decreasing ground clearance led to a reduction in CL at 0\u00b0, whereas it caused an increase at 4\u00b0 and 8\u00b0.<\/p>\n

DOI:<\/strong> https:\/\/doi.org\/10.58559\/ijes.1797420<\/a><\/p>\n

Makale Sayfas\u0131:<\/strong> DergiPark ba\u011flant\u0131s\u0131<\/a><\/p>\n

Tam Metin (PDF):<\/strong> PDF indir<\/a><\/p>\n

\n

Kategori:<\/em> Hakemli<\/p>\n","protected":false},"excerpt":{"rendered":"

In the present study, an examination of the aerodynamic characteristics in tandem airfoil systems experiencing ground effect was performed. The research was carried out using Computational Fluid Dynamics (CFD) analyses. The effects of multiple parameters, such as angle of attack (AOA) at 0\u00b0, 4\u00b0, and\u2026<\/p>\n","protected":false},"author":241,"featured_media":0,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"_thinkrank_schema_form_data":"","_thinkrank_selected_schema_type":"","_thinkrank_additional_schemas":"","_thinkrank_canonical_url":"","_thinkrank_og_title":"","_thinkrank_og_description":"","_thinkrank_og_image":"","_thinkrank_twitter_title":"","_thinkrank_twitter_description":"","_thinkrank_twitter_image":"","_thinkrank_imported_from":"","_thinkrank_focus_keywords":[],"_thinkrank_focus_keyword":"","_thinkrank_robots_meta_enabled":0,"_thinkrank_robots_meta":"","_thinkrank_advanced_robots_meta":"","_thinkrank_primary_category":0,"footnotes":"","_ppma_block_editor_authors":""},"categories":[2346],"tags":[],"ppma_author":[2347],"class_list":["post-2332972625","post","type-post","status-publish","format-standard","hentry","category-hakemli"],"yoast_head":"\nCFD analysis of lift, drag, and moment coefficients of a tandem airfoil under ground effect - T\u00fcrkiye Enerji Stratejileri ve Politikalar\u0131 Ara\u015ft\u0131rma Merkezi<\/title>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/www.tespam.org\/wordpress\/cfd-analysis-of-lift-drag-and-moment-coefficients-of-a-tandem-airfoil-under-ground-effect\/\" \/>\n<meta property=\"og:locale\" content=\"tr_TR\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"CFD analysis of lift, drag, and moment coefficients of a tandem airfoil under ground effect - T\u00fcrkiye Enerji Stratejileri ve Politikalar\u0131 Ara\u015ft\u0131rma Merkezi\" \/>\n<meta property=\"og:description\" content=\"In the present study, an examination of the aerodynamic characteristics in tandem airfoil systems experiencing ground effect was performed. 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