{"id":561,"date":"2022-03-10T12:28:18","date_gmt":"2022-03-10T11:28:18","guid":{"rendered":"https:\/\/people.unipi.it\/vittorio_cipolla\/?p=561"},"modified":"2022-09-25T15:11:29","modified_gmt":"2022-09-25T13:11:29","slug":"a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom","status":"publish","type":"post","link":"https:\/\/people.unipi.it\/vittorio_cipolla\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\/","title":{"rendered":"A new paper published in Journal of Aerospace Engineering (ASCE): \u201cPrediction of maximum lift coefficient of box-wing aircraft through the combination of an analytical adaptation of the DATCOM method and Vortex-Lattice simulations\u201d"},"content":{"rendered":"\r\n<ul class=\"wp-block-gallery columns-3 is-cropped wp-block-gallery-1 is-layout-flex wp-block-gallery-is-layout-flex\">\r\n<li class=\"blocks-gallery-item\">\r\n<figure><a href=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/REND-06-ABOVE-CLOUDS-scaled.jpg\"><img loading=\"lazy\" decoding=\"async\" class=\"alignnone size-medium wp-image-387\" src=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/REND-06-ABOVE-CLOUDS-300x184.jpg\" alt=\"\" width=\"300\" height=\"184\" srcset=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/REND-06-ABOVE-CLOUDS-300x184.jpg 300w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/REND-06-ABOVE-CLOUDS-1024x628.jpg 1024w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/REND-06-ABOVE-CLOUDS-768x471.jpg 768w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/REND-06-ABOVE-CLOUDS-1536x942.jpg 1536w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/REND-06-ABOVE-CLOUDS-2048x1256.jpg 2048w\" sizes=\"auto, (max-width: 300px) 100vw, 300px\" \/><\/a><\/figure>\r\n<\/li>\r\n<li class=\"blocks-gallery-item\">\r\n<figure><a href=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2022\/03\/CLMAX-1.png\"><img loading=\"lazy\" decoding=\"async\" class=\"alignnone size-medium wp-image-626\" src=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2022\/03\/CLMAX-1-300x185.png\" alt=\"\" width=\"300\" height=\"185\" srcset=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2022\/03\/CLMAX-1-300x185.png 300w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2022\/03\/CLMAX-1-1024x630.png 1024w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2022\/03\/CLMAX-1-768x473.png 768w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2022\/03\/CLMAX-1.png 1147w\" sizes=\"auto, (max-width: 300px) 100vw, 300px\" \/><\/a><br \/>\u00a0<\/figure>\r\n<\/li>\r\n<\/ul>\r\n\r\n\r\n\r\n<p class=\"StyleAbstractLinespacingDouble1 wp-block-paragraph\" style=\"margin-top: 0cm\"><span lang=\"EN-US\">The present paper concerns the introduction of a mixed analytical-numerical method for the estimation of the maximum lift coefficient of box-wing aircraft in unflapped configuration. The analytical aspect is related to the adaptation of the DATCOM method by means of an approach built on the characteristics of the optimal lift distribution of the box-wing and implemented through simplifying assumptions. Since the formulation depends on parameters proper of the considered aircraft, numerical simulations are performed through a Vortex-Lattice Method to complete the input dataset. The method is first presented and then validated for the case of the 2-seater amphibious PrandtlPlane from the project \u201cIDINTOS\u201d, for which wind tunnel data are available. The method is then applied to two test cases for which CFD data are available: a 300 passengers mid-range PrandtlPlane, developed within the European research project \u201cPARSIFAL\u201d, and a regional hybrid-electric PrandtlPlane, object of study in the Italian research project \u201cPROSIB\u201d. Results are presented and discussed, also analyzing the links between the proposed method and relevant parameters of the box-wing design, such as taper ratios and wing loading repartition among the two wings.<\/span><\/p>\r\n\r\n\r\n\r\n<h4 class=\"wp-block-heading\">Cite and Share<\/h4>\r\n\r\n\r\n\r\n<p class=\"wp-block-paragraph\">Cipolla, V., Abu Salem, K., Palaia, G., Binante, V., Zanetti, D. (2022). <em>Prediction of Maximum Lift Coefficient of Box-Wing Aircraft through the Combination of an Analytical Adaptation of the DATCOM Method and Vortex-Lattice Simulations.<\/em> JOURNAL OF AEROSPACE ENGINEERING, vol. 35, p. 1-13. doi: 10.1061\/(ASCE)AS.1943-5525.0001409<\/p>\r\n\r\n\r\n\r\n<p class=\"wp-block-paragraph\">Full-text here: <a href=\"https:\/\/ascelibrary.org\/doi\/full\/10.1061\/(ASCE)AS.1943-5525.0001409\" target=\"_blank\" rel=\"noopener\">https:\/\/ascelibrary.org\/doi\/full\/10.1061\/(ASCE)AS.1943-5525.0001409<\/a><\/p>\r\n\r\n<p><a href=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/1200px-Open_Access_logo_PLoS_transparent.svg_-2.png\"><img loading=\"lazy\" decoding=\"async\" class=\"wp-image-59 alignnone\" src=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/1200px-Open_Access_logo_PLoS_transparent.svg_-2-192x300.png\" alt=\"\" width=\"47\" height=\"73\" srcset=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/1200px-Open_Access_logo_PLoS_transparent.svg_-2-192x300.png 192w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/1200px-Open_Access_logo_PLoS_transparent.svg_-2-655x1024.png 655w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/1200px-Open_Access_logo_PLoS_transparent.svg_-2-768x1200.png 768w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/1200px-Open_Access_logo_PLoS_transparent.svg_-2-983x1536.png 983w, https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/11\/1200px-Open_Access_logo_PLoS_transparent.svg_-2.png 1200w\" sizes=\"auto, (max-width: 47px) 100vw, 47px\" \/><\/a>Open-acces accepted version available on <a href=\"https:\/\/www.researchgate.net\/publication\/359134787_Prediction_of_Maximum_Lift_Coefficient_of_Box-Wing_Aircraft_through_the_Combination_of_an_Analytical_Adaptation_of_the_DATCOM_Method_and_Vortex-Lattice_Simulations\" target=\"_blank\" rel=\"noopener\">Reaserch Gate<\/a><\/p>","protected":false},"excerpt":{"rendered":"<p>The present paper concerns the introduction of a mixed analytical-numerical method for the estimation of the maximum lift coefficient of box-wing aircraft in unflapped configuration. The analytical aspect is related to the adaptation of the DATCOM method by means of an approach built on the characteristics of the optimal lift distribution of the box-wing and [&hellip;]<\/p>\n","protected":false},"author":636,"featured_media":568,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"footnotes":""},"categories":[14,15,9,10,11],"tags":[16,18,19,49,28,29,31,33],"class_list":["post-561","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-idintos","category-parsifal","category-projects","category-prosib","category-publications","tag-aerodynamics","tag-aircraft-design","tag-box-wing","tag-idintos","tag-parsifal","tag-prandtlplane","tag-prosib","tag-research"],"acf":[],"featured_image_src":"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/12\/ASCE_JoAE.jpg","author_info":{"display_name":"Cipolla V.","author_link":"https:\/\/people.unipi.it\/vittorio_cipolla\/author\/a013084\/"},"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v28.4 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>A new paper published in Journal of Aerospace Engineering (ASCE): \u201cPrediction of maximum lift coefficient of box-wing aircraft through the combination of an analytical adaptation of the DATCOM method and Vortex-Lattice simulations\u201d - Vittorio Cipolla<\/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:\/\/people.unipi.it\/vittorio_cipolla\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\/\" \/>\n<meta property=\"og:locale\" content=\"en_US\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"A new paper published in Journal of Aerospace Engineering (ASCE): \u201cPrediction of maximum lift coefficient of box-wing aircraft through the combination of an analytical adaptation of the DATCOM method and Vortex-Lattice simulations\u201d - Vittorio Cipolla\" \/>\n<meta property=\"og:description\" content=\"The present paper concerns the introduction of a mixed analytical-numerical method for the estimation of the maximum lift coefficient of box-wing aircraft in unflapped configuration. The analytical aspect is related to the adaptation of the DATCOM method by means of an approach built on the characteristics of the optimal lift distribution of the box-wing and [&hellip;]\" \/>\n<meta property=\"og:url\" content=\"https:\/\/people.unipi.it\/vittorio_cipolla\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\/\" \/>\n<meta property=\"og:site_name\" content=\"Vittorio Cipolla\" \/>\n<meta property=\"article:published_time\" content=\"2022-03-10T11:28:18+00:00\" \/>\n<meta property=\"article:modified_time\" content=\"2022-09-25T13:11:29+00:00\" \/>\n<meta property=\"og:image\" content=\"https:\/\/people.unipi.it\/vittorio_cipolla\/wp-content\/uploads\/sites\/603\/2021\/12\/ASCE_JoAE.jpg\" \/>\n\t<meta property=\"og:image:width\" content=\"771\" \/>\n\t<meta property=\"og:image:height\" content=\"100\" \/>\n\t<meta property=\"og:image:type\" content=\"image\/jpeg\" \/>\n<meta name=\"author\" content=\"Cipolla V.\" \/>\n<meta name=\"twitter:card\" content=\"summary_large_image\" \/>\n<meta name=\"twitter:label1\" content=\"Written by\" \/>\n\t<meta name=\"twitter:data1\" content=\"Cipolla V.\" \/>\n\t<meta name=\"twitter:label2\" content=\"Est. reading time\" \/>\n\t<meta name=\"twitter:data2\" content=\"1 minute\" \/>\n<script type=\"application\/ld+json\" class=\"yoast-schema-graph\">{\"@context\":\"https:\\\/\\\/schema.org\",\"@graph\":[{\"@type\":\"Article\",\"@id\":\"https:\\\/\\\/people.unipi.it\\\/vittorio_cipolla\\\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\\\/#article\",\"isPartOf\":{\"@id\":\"https:\\\/\\\/people.unipi.it\\\/vittorio_cipolla\\\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\\\/\"},\"author\":{\"name\":\"Cipolla V.\",\"@id\":\"https:\\\/\\\/people.unipi.it\\\/vittorio_cipolla\\\/#\\\/schema\\\/person\\\/ea3f46a21248a6b50ef27bc143bce6f4\"},\"headline\":\"A new paper published in Journal of Aerospace Engineering (ASCE): \u201cPrediction of maximum lift coefficient of box-wing aircraft through the combination of an analytical adaptation of the DATCOM method and Vortex-Lattice simulations\u201d\",\"datePublished\":\"2022-03-10T11:28:18+00:00\",\"dateModified\":\"2022-09-25T13:11:29+00:00\",\"mainEntityOfPage\":{\"@id\":\"https:\\\/\\\/people.unipi.it\\\/vittorio_cipolla\\\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\\\/\"},\"wordCount\":278,\"image\":{\"@id\":\"https:\\\/\\\/people.unipi.it\\\/vittorio_cipolla\\\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\\\/#primaryimage\"},\"thumbnailUrl\":\"https:\\\/\\\/people.unipi.it\\\/vittorio_cipolla\\\/wp-content\\\/uploads\\\/sites\\\/603\\\/2021\\\/12\\\/ASCE_JoAE.jpg\",\"keywords\":[\"Aerodynamics\",\"Aircraft Design\",\"Box-wing\",\"IDINTOS\",\"PARSIFAL\",\"PrandtlPlane\",\"PROSIB\",\"Research\"],\"articleSection\":[\"IDINTOS\",\"PARSIFAL\",\"Projects\",\"PROSIB\",\"Publications\"],\"inLanguage\":\"en-AU\"},{\"@type\":\"WebPage\",\"@id\":\"https:\\\/\\\/people.unipi.it\\\/vittorio_cipolla\\\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\\\/\",\"url\":\"https:\\\/\\\/people.unipi.it\\\/vittorio_cipolla\\\/a-new-paper-published-in-journal-of-aerospace-engineering-asce-prediction-of-maximum-lift-coefficient-of-box-wing-aircraft-through-the-combination-of-an-analytical-adaptation-of-the-datcom\\\/\",\"name\":\"A new paper published in Journal of Aerospace Engineering (ASCE): \u201cPrediction of maximum lift coefficient of box-wing aircraft through the combination of an analytical adaptation of the DATCOM method and Vortex-Lattice simulations\u201d - 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