{"id":3422,"date":"2017-05-30T19:19:05","date_gmt":"2017-05-30T16:19:05","guid":{"rendered":"https:\/\/inginerie.aero\/?p=3422"},"modified":"2017-05-30T19:19:05","modified_gmt":"2017-05-30T16:19:05","slug":"aerospace-structures-laboratory","status":"publish","type":"post","link":"https:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/","title":{"rendered":"Aerospace Structures Laboratory"},"content":{"rendered":"<p>[et_pb_section admin_label=&#8221;section&#8221;][et_pb_row admin_label=&#8221;row&#8221;][et_pb_column type=&#8221;4_4&#8243;][et_pb_text admin_label=&#8221;Text&#8221; background_layout=&#8221;light&#8221; text_orientation=&#8221;left&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;]<\/p>\n<p>&nbsp;<\/p>\n<h3><span id=\"result_box\" lang=\"en\" tabindex=\"-1\">Equipping the Aerospace Structure Laboratory with an AG6 aircraft<\/span><span id=\"t-served-community-button\" class=\"trans-verified-button goog-toolbar-button\"><\/span><\/h3>\n<p><span id=\"result_box\" lang=\"en\" tabindex=\"-1\">The Faculty of Aerospace Engineering wishes to warmly thank the management and staff of AEROSTAR S.A. Bacau that contributed to the endowment of the Aerospace Structures Laboratory by donating a utility aircraft type AG-6. We also thank EUROAVIA members and other students who participated in (re) assembling the aircraft in the Aerospace Structures Laboratory.<\/span><span id=\"t-served-community-button\" class=\"trans-verified-button goog-toolbar-button\"><\/span><\/p>\n<p>AG-6 aircraft (<a href=\"http:\/\/www.inav.ro\/aeronautica_ag6.php\" target=\"_blank\" rel=\"noopener noreferrer\">http:\/\/www.inav.ro\/aeronautica_ag6.php<\/a>) i<span id=\"result_box\" lang=\"en\" tabindex=\"-1\">s a biplan designed specifically for spraying or sowing agricultural materials from very low and low altitude, practically for any type of field. The aircraft has a non-load bearing type structure, the fuselage being a lattice-like structure (Fig. 1). The wings of the biplan have metal struts, the extras and the attack board being metallic, while the intrados is studded. The landing\u00a0gear is tall, with a damper on the main train, ensuring take-off and landing on any terrain. <\/span><span id=\"t-served-community-button\" class=\"trans-verified-button goog-toolbar-button\"><\/span><\/p>\n<p>&nbsp;<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][et_pb_row admin_label=&#8221;R\u00e2nd&#8221;][et_pb_column type=&#8221;1_3&#8243;][et_pb_image admin_label=&#8221;Imagine&#8221; src=&#8221;https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa5.jpg&#8221; alt=&#8221;Imagini (selec\u021bie) din timpul reasambl\u0103rii aeronavei sub coordonarea unei echipe de tehnicieni de la AEROSTAR Bac\u0103u&#8221; title_text=&#8221;Imagini (selec\u021bie) din timpul reasambl\u0103rii aeronavei sub coordonarea unei echipe de tehnicieni de la AEROSTAR Bac\u0103u&#8221; show_in_lightbox=&#8221;off&#8221; url_new_window=&#8221;off&#8221; use_overlay=&#8221;off&#8221; animation=&#8221;left&#8221; sticky=&#8221;off&#8221; align=&#8221;left&#8221; force_fullwidth=&#8221;off&#8221; always_center_on_mobile=&#8221;on&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;] [\/et_pb_image][\/et_pb_column][et_pb_column type=&#8221;1_3&#8243;][et_pb_image admin_label=&#8221;Imagine&#8221; src=&#8221;https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa4.jpg&#8221; alt=&#8221;Imagini (selec\u021bie) din timpul reasambl\u0103rii aeronavei sub coordonarea unei echipe de tehnicieni de la AEROSTAR Bac\u0103u&#8221; title_text=&#8221;Imagini (selec\u021bie) din timpul reasambl\u0103rii aeronavei sub coordonarea unei echipe de tehnicieni de la AEROSTAR Bac\u0103u&#8221; show_in_lightbox=&#8221;off&#8221; url_new_window=&#8221;off&#8221; use_overlay=&#8221;off&#8221; animation=&#8221;left&#8221; sticky=&#8221;off&#8221; align=&#8221;left&#8221; force_fullwidth=&#8221;off&#8221; always_center_on_mobile=&#8221;on&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;] [\/et_pb_image][\/et_pb_column][et_pb_column type=&#8221;1_3&#8243;][et_pb_image admin_label=&#8221;Imagine&#8221; src=&#8221;https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa1.jpg&#8221; show_in_lightbox=&#8221;off&#8221; url_new_window=&#8221;off&#8221; use_overlay=&#8221;off&#8221; animation=&#8221;left&#8221; sticky=&#8221;off&#8221; align=&#8221;left&#8221; force_fullwidth=&#8221;off&#8221; always_center_on_mobile=&#8221;on&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;] [\/et_pb_image][\/et_pb_column][\/et_pb_row][et_pb_row admin_label=&#8221;R\u00e2nd&#8221;][et_pb_column type=&#8221;4_4&#8243;][et_pb_text admin_label=&#8221;Text&#8221; background_layout=&#8221;light&#8221; text_orientation=&#8221;left&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;]<\/p>\n<p>&nbsp;<\/p>\n<p align=\"JUSTIFY\"><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"Cabina monoloc este echipat\u0103 standard cu toate instrumentele de naviga\u021bie \u0219i de control necesare.\">The single seat\u00a0cockpit is equipped with all necessary navigation and control instruments. <\/span><span title=\"Fiind supra\u00een\u0103l\u021bat\u0103, cu ample suprafe\u021be vitrate, cabina ofer\u0103 o bun\u0103 vizibilitate pilotului.\">Being elevated, with plenty of\u00a0glass surfaces, the <span style=\"color: #656565; font-family: Tahoma; font-size: small;\">cockpit<\/span> offers good visibility to the pilot. <\/span><span title=\"Aeronava este extrem de manevrabila si are un motor de tip radial M-14P ce dezvolt\u0103 o putere de 360 CP (motorul echipeaz\u0103 \u0219i avionul Yak-52), trac\u021biunea fiind asigurat\u0103 de o elice tripal\u0103 cu pas variabil.\">The aircraft is highly manoeuvrable and has a M-14P radial engine that develops 360 hp (the same engine also equips the Yak-52), the traction being ensured by a variable pitch triple propeller. <\/span><span title=\"Solu\u021bia de tip biplan \u0219i repriza scurt\u0103 a motorului sunt avantajele principale ale avionului.\">The biplan solution and the short engine half are the main advantages of the aircraft. <\/span><span title=\"Manevrabilitatea este important\u0103 pentru viraje str\u00e2nse \u00een jurul sau peste obstacole \u00een condi\u021bii de siguran\u021b\u0103, \u00een timp ce repriza scurt\u0103 a motorului asigur\u0103 urcarea rapid\u0103 la altitudine \u00een cazul terenurilor cu obstacole.\">Maneuverability is important for tight turns around or over obstacles in a safe way, while the\u00a0agile engine ensures fast\u00a0climbing over unanticipated obstacle. <\/span><span title=\"Prototipul aeronavei AG6 a fost fabricat la AEROSTAR Bac\u0103u, unde a \u0219i efectuat primul zbor \u00een ziua de 12 ianuarie 1989. Acest prototip semifunc\u021bional este folosit acum \u00een procesul didactic \u00een cadrul facult\u0103\u021bii.\n\n\">The prototype of the AG6 aircraft was manufactured\u00a0by AEROSTAR Bacau, where it made its first flight on January 12, 1989. This semifunctional prototype is now used in the teaching process within the faculty.<\/p>\n<p><\/span><span title=\"Date tehnice:\n\"><strong>Technical data:<\/strong><\/span><\/span><\/span><\/span><\/span><\/p>\n<ul>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022anvergura (plan superior) 12.46 m\n\">wing span\u00a012.46 m<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022coarda (constant\u0103) 1.5 m\n\">aerodynamic chord\u00a01.5 m<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022greutatea de baz\u0103 certificat\u0103 2700 kg (FAR-23 NORMAL)\n\">certified base weight 2700 kg (FAR-23 NORMAL)<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022greutatea maxim\u0103 de decolare 3200 kg\n\">maximum take-off weight 3200 kg<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022viteza ce nu trebuie dep\u0103\u0219it\u0103 255 km\/h\n\">speed \u200b\u200bnot to be exceed 255 km\/h<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022viteza maxim\u0103 de croazier\u0103 195 km\/h\n\">maximum cruising speed of 195 km\/h<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022viteza de operare pentru pulverizare substan\u021be 185 km\/h\n\">maximum operating speed for spraying substances 185 km\/h<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022viteza de angajare cu motorul oprit 95 km\/h\n\">stall\u00a0speed (with the engine stopped) 95 km\/h<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022rata de urcare 300 m\/min\n\">climbing rate 300 m\/min<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022distan\u021ba de rulare la decolare 150 m\n\">take-off distance 150 m<\/span><\/span><\/span><\/span><\/span><\/li>\n<li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><span id=\"result_box\" lang=\"en\" tabindex=\"-1\"><span title=\"\u2022distan\u021ba de rulare la aterizare 180 m.\">landing distance 180 m.<\/span><\/span><span id=\"t-served-community-button\" class=\"trans-verified-button goog-toolbar-button\"><\/span><\/span><\/span><\/span><\/li>\n<\/ul>\n<p>&nbsp;<\/p>\n<p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][et_pb_row admin_label=&#8221;R\u00e2nd&#8221;][et_pb_column type=&#8221;1_3&#8243;][et_pb_image admin_label=&#8221;Imagine&#8221; src=&#8221;https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa3.jpg&#8221; show_in_lightbox=&#8221;off&#8221; url_new_window=&#8221;off&#8221; use_overlay=&#8221;off&#8221; animation=&#8221;left&#8221; sticky=&#8221;off&#8221; align=&#8221;left&#8221; force_fullwidth=&#8221;off&#8221; always_center_on_mobile=&#8221;on&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;] [\/et_pb_image][\/et_pb_column][et_pb_column type=&#8221;2_3&#8243;][et_pb_image admin_label=&#8221;Imagine&#8221; src=&#8221;https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa6.jpg&#8221; show_in_lightbox=&#8221;off&#8221; url_new_window=&#8221;off&#8221; use_overlay=&#8221;off&#8221; animation=&#8221;left&#8221; sticky=&#8221;off&#8221; align=&#8221;left&#8221; force_fullwidth=&#8221;off&#8221; always_center_on_mobile=&#8221;on&#8221; use_border_color=&#8221;off&#8221; border_color=&#8221;#ffffff&#8221; border_style=&#8221;solid&#8221;] [\/et_pb_image][\/et_pb_column][\/et_pb_row][\/et_pb_section]<\/p>\n","protected":false},"excerpt":{"rendered":"<p>&nbsp; Equipping the Aerospace Structure Laboratory with an AG6 aircraft The Faculty of Aerospace Engineering wishes to warmly thank the management and staff of AEROSTAR S.A. Bacau that contributed to the endowment of the Aerospace Structures Laboratory by donating a utility aircraft type AG-6. We also thank EUROAVIA members and other students who participated in [&hellip;]<\/p>\n","protected":false},"author":6,"featured_media":1554,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"_et_pb_use_builder":"on","_et_pb_old_content":"<p>[et_pb_section admin_label=\"section\"][et_pb_row admin_label=\"row\"][et_pb_column type=\"4_4\"][et_pb_text admin_label=\"Text\" background_layout=\"light\" text_orientation=\"left\" use_border_color=\"off\" border_color=\"#ffffff\" border_style=\"solid\"]<\/p><h3>Dotarea Laboratorului de Structuri Aerospatiale cu o aeronava AG6<\/h3><p>Facultatea de Inginerie Aerospa\u021bial\u0103 dore\u0219te s\u0103 mul\u021bumeasc\u0103 c\u0103lduros conducerii \u0219i personalului companiei AEROSTAR S.A. Bac\u0103u care a contribuit la dotarea Laboratorului de Structuri Aerospatiale din cadrul facult\u0103\u021bii prin donarea unei aeronave utilitare de tip AG-6. Multumim de asemenea membrilor EUROAVIA si celorla\u021bi studen\u021bi care au participat la (re)asamblarea aeronavei in Laboratorul de Structuri Aerospatiale.<\/p><p>Avionul AG-6 (<a href=\"http:\/\/www.inav.ro\/aeronautica_ag6.php\" target=\"_blank\" rel=\"noopener noreferrer\">http:\/\/www.inav.ro\/aeronautica_ag6.php<\/a>) este un biplan proiectat special pentru stropire, pulverizare sau \u00eens\u0103m\u00e2n\u021barea de materiale agricole de la altitudine foarte joas\u0103 \u0219i joas\u0103, practic pentru orice tip de teren. Aeronava are o structur\u0103 de rezisten\u021b\u0103 de tip f\u0103r\u0103 \u00eenveli\u0219 portant, fuselajul fiind o construc\u021bie de tip grind\u0103 cu z\u0103brele (fig.1). Aripile biplanului au lonjeroane metalice, extradosul \u0219i bordul de atac fiind metalic, \u00een timp ce intradosul este \u00eemp\u00e2nzit. Trenul de aterizare este \u00eenalt, cu amortizor pe trenul principal, asigur\u00e2nd decolarea \u0219i aterizarea pe teren neamenajat.<\/p><p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][et_pb_row admin_label=\"R\u00e2nd\"][et_pb_column type=\"1_3\"][et_pb_image admin_label=\"Imagine\" src=\"https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa5.jpg\" alt=\"Imagini (selec\u021bie) din timpul reasambl\u0103rii aeronavei sub coordonarea unei echipe de tehnicieni de la AEROSTAR Bac\u0103u\" title_text=\"Imagini (selec\u021bie) din timpul reasambl\u0103rii aeronavei sub coordonarea unei echipe de tehnicieni de la AEROSTAR Bac\u0103u\" show_in_lightbox=\"off\" url_new_window=\"off\" use_overlay=\"off\" animation=\"left\" sticky=\"off\" align=\"left\" force_fullwidth=\"off\" always_center_on_mobile=\"on\" use_border_color=\"off\" border_color=\"#ffffff\" border_style=\"solid\" \/][\/et_pb_column][et_pb_column type=\"1_3\"][et_pb_image admin_label=\"Imagine\" src=\"https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa4.jpg\" alt=\"Imagini (selec\u021bie) din timpul reasambl\u0103rii aeronavei sub coordonarea unei echipe de tehnicieni de la AEROSTAR Bac\u0103u\" title_text=\"Imagini (selec\u021bie) din timpul reasambl\u0103rii aeronavei sub coordonarea unei echipe de tehnicieni de la AEROSTAR Bac\u0103u\" show_in_lightbox=\"off\" url_new_window=\"off\" use_overlay=\"off\" animation=\"left\" sticky=\"off\" align=\"left\" force_fullwidth=\"off\" always_center_on_mobile=\"on\" use_border_color=\"off\" border_color=\"#ffffff\" border_style=\"solid\" \/][\/et_pb_column][et_pb_column type=\"1_3\"][et_pb_image admin_label=\"Imagine\" src=\"https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa1.jpg\" show_in_lightbox=\"off\" url_new_window=\"off\" use_overlay=\"off\" animation=\"left\" sticky=\"off\" align=\"left\" force_fullwidth=\"off\" always_center_on_mobile=\"on\" use_border_color=\"off\" border_color=\"#ffffff\" border_style=\"solid\" \/][\/et_pb_column][\/et_pb_row][et_pb_row admin_label=\"R\u00e2nd\"][et_pb_column type=\"4_4\"][et_pb_text admin_label=\"Text\" background_layout=\"light\" text_orientation=\"left\" use_border_color=\"off\" border_color=\"#ffffff\" border_style=\"solid\"]<\/p><p align=\"JUSTIFY\"><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">Cabina monoloc este echipat\u0103 standard cu toate instrumentele de naviga\u021bie \u0219i de control necesare. Fiind supra\u00een\u0103l\u021bat\u0103, cu ample suprafe\u021be vitrate, cabina ofer\u0103 o bun\u0103 vizibilitate pilotului. Aeronava este extrem de manevrabila si are un motor de tip radial M-14P ce dezvolt\u0103 o putere de 360 CP (motorul echipeaz\u0103 \u0219i avionul Yak-52), trac\u021biunea fiind asigurat\u0103 de o elice tripal\u0103 cu pas variabil. Solu\u021bia de tip biplan \u0219i repriza scurt\u0103 a motorului sunt avantajele principale ale avionului. Manevrabilitatea este important\u0103 pentru viraje str\u00e2nse \u00een jurul sau peste obstacole \u00een condi\u021bii de siguran\u021b\u0103, \u00een timp ce repriza scurt\u0103 a motorului asigur\u0103 urcarea rapid\u0103 la altitudine \u00een cazul terenurilor cu obstacole. Prototipul aeronavei AG6 a fost fabricat la AEROSTAR Bac\u0103u, unde a \u0219i efectuat primul zbor \u00een ziua de 12 ianuarie 1989. Acest prototip semifunc\u021bional este folosit acum \u00een procesul didactic \u00een cadrul facult\u0103\u021bii.<\/span><\/span><\/span><\/p><p><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\"><b>Date tehnice:<\/b><\/span><\/span><\/span><\/p><ul><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">anvergura (plan superior) 12.46 m<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">coarda (constant\u0103) 1.5 m<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">greutatea de baz\u0103 certificat\u0103 2700 kg (FAR-23 NORMAL)<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">greutatea maxim\u0103 de decolare 3200 kg<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">viteza ce nu trebuie dep\u0103\u0219it\u0103 255 km\/h<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">viteza maxim\u0103 de croazier\u0103 195 km\/h<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">viteza de operare pentru pulverizare substan\u021be 185 km\/h<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">viteza de angajare cu motorul oprit 95 km\/h<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">rata de urcare 300 m\/min<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">distan\u021ba de rulare la decolare 150 m<\/span><\/span><\/span><\/li><li><span style=\"color: #656565;\"><span style=\"font-family: Tahoma, serif;\"><span style=\"font-size: small;\">distan\u021ba de rulare la aterizare 180 m.<\/span><\/span><\/span><\/li><\/ul><p>[\/et_pb_text][\/et_pb_column][\/et_pb_row][et_pb_row admin_label=\"R\u00e2nd\"][et_pb_column type=\"1_3\"][et_pb_image admin_label=\"Imagine\" src=\"https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa3.jpg\" show_in_lightbox=\"off\" url_new_window=\"off\" use_overlay=\"off\" animation=\"left\" sticky=\"off\" align=\"left\" force_fullwidth=\"off\" always_center_on_mobile=\"on\" use_border_color=\"off\" border_color=\"#ffffff\" border_style=\"solid\" \/][\/et_pb_column][et_pb_column type=\"2_3\"][et_pb_image admin_label=\"Imagine\" src=\"https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa6.jpg\" show_in_lightbox=\"off\" url_new_window=\"off\" use_overlay=\"off\" animation=\"left\" sticky=\"off\" align=\"left\" force_fullwidth=\"off\" always_center_on_mobile=\"on\" use_border_color=\"off\" border_color=\"#ffffff\" border_style=\"solid\" \/][\/et_pb_column][\/et_pb_row][\/et_pb_section]<\/p>","_et_gb_content_width":"","jetpack_post_was_ever_published":false,"_jetpack_newsletter_access":"","_jetpack_dont_email_post_to_subs":false,"_jetpack_newsletter_tier_id":0,"_jetpack_memberships_contains_paywalled_content":false,"_jetpack_memberships_contains_paid_content":false,"footnotes":"","jetpack_publicize_message":"","jetpack_publicize_feature_enabled":true,"jetpack_social_post_already_shared":true,"jetpack_social_options":{"image_generator_settings":{"template":"highway","enabled":false},"version":2},"_links_to":"","_links_to_target":""},"categories":[131],"tags":[],"class_list":["post-3422","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-laboratories"],"jetpack_publicize_connections":[],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v24.3 - https:\/\/yoast.com\/wordpress\/plugins\/seo\/ -->\n<title>Aerospace Structures Laboratory - Alumni Politehnica Aerospace Engineering<\/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:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/\" \/>\n<meta property=\"og:locale\" content=\"ro_RO\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Aerospace Structures Laboratory - Alumni Politehnica Aerospace Engineering\" \/>\n<meta property=\"og:description\" content=\"&nbsp; Equipping the Aerospace Structure Laboratory with an AG6 aircraft The Faculty of Aerospace Engineering wishes to warmly thank the management and staff of AEROSTAR S.A. Bacau that contributed to the endowment of the Aerospace Structures Laboratory by donating a utility aircraft type AG-6. We also thank EUROAVIA members and other students who participated in [&hellip;]\" \/>\n<meta property=\"og:url\" content=\"https:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/\" \/>\n<meta property=\"og:site_name\" content=\"Alumni Politehnica Aerospace Engineering\" \/>\n<meta property=\"article:publisher\" content=\"https:\/\/www.facebook.com\/groups\/InginerieAerospatiala\/\" \/>\n<meta property=\"article:published_time\" content=\"2017-05-30T16:19:05+00:00\" \/>\n<meta property=\"og:image\" content=\"https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa2.jpg\" \/>\n\t<meta property=\"og:image:width\" content=\"701\" \/>\n\t<meta property=\"og:image:height\" content=\"516\" \/>\n\t<meta property=\"og:image:type\" content=\"image\/jpeg\" \/>\n<meta name=\"author\" content=\"Cristian Emil Constantinescu\" \/>\n<meta name=\"twitter:card\" content=\"summary_large_image\" \/>\n<meta name=\"twitter:label1\" content=\"Scris de\" \/>\n\t<meta name=\"twitter:data1\" content=\"Cristian Emil Constantinescu\" \/>\n\t<meta name=\"twitter:label2\" content=\"Timp estimat pentru citire\" \/>\n\t<meta name=\"twitter:data2\" content=\"4 minute\" \/>\n<script type=\"application\/ld+json\" class=\"yoast-schema-graph\">{\"@context\":\"https:\/\/schema.org\",\"@graph\":[{\"@type\":\"Article\",\"@id\":\"https:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/#article\",\"isPartOf\":{\"@id\":\"https:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/\"},\"author\":{\"name\":\"Cristian Emil Constantinescu\",\"@id\":\"https:\/\/inginerie.aero\/#\/schema\/person\/e915a4f6c4ecd239b38196102b96b36e\"},\"headline\":\"Aerospace Structures Laboratory\",\"datePublished\":\"2017-05-30T16:19:05+00:00\",\"dateModified\":\"2017-05-30T16:19:05+00:00\",\"mainEntityOfPage\":{\"@id\":\"https:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/\"},\"wordCount\":840,\"publisher\":{\"@id\":\"https:\/\/inginerie.aero\/#organization\"},\"image\":{\"@id\":\"https:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/#primaryimage\"},\"thumbnailUrl\":\"https:\/\/inginerie.aero\/wp-content\/uploads\/2017\/04\/lab_sa2.jpg\",\"articleSection\":[\"Laboratories\"],\"inLanguage\":\"ro-RO\"},{\"@type\":\"WebPage\",\"@id\":\"https:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/\",\"url\":\"https:\/\/inginerie.aero\/index.php\/en\/2017\/05\/30\/aerospace-structures-laboratory\/\",\"name\":\"Aerospace Structures Laboratory - 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