[{"data":1,"prerenderedAt":-1},["ShallowReactive",2],{"detail-sidebar-cat-0-en-105":3,"doc-seo-181296-105":59,"doc-detail-181296-en":131},{"code":4,"msg":5,"data":6},0,"success",[7,13,18,23,28,33,38,43,48,51,55],{"id":8,"doc_module":4,"doc_module_name":9,"category_name":10,"show_sort_weight":11,"slug":12},1,"Document","Story & Novel",90,"story-novel",{"id":14,"doc_module":4,"doc_module_name":9,"category_name":15,"show_sort_weight":16,"slug":17},2,"Literature",80,"literature",{"id":19,"doc_module":4,"doc_module_name":9,"category_name":20,"show_sort_weight":21,"slug":22},4,"Exam",70,"exam",{"id":24,"doc_module":4,"doc_module_name":9,"category_name":25,"show_sort_weight":26,"slug":27},5,"Comic",60,"comic",{"id":29,"doc_module":4,"doc_module_name":9,"category_name":30,"show_sort_weight":31,"slug":32},6,"Technology",50,"technology",{"id":34,"doc_module":4,"doc_module_name":9,"category_name":35,"show_sort_weight":36,"slug":37},7,"Healthcare",40,"healthcare",{"id":39,"doc_module":4,"doc_module_name":9,"category_name":40,"show_sort_weight":41,"slug":42},8,"Research & Report",30,"research-report",{"id":44,"doc_module":4,"doc_module_name":9,"category_name":45,"show_sort_weight":46,"slug":47},9,"Religion & Spirituality",20,"religion-spirituality",{"id":46,"doc_module":4,"doc_module_name":9,"category_name":49,"show_sort_weight":46,"slug":50},"World Cup","world-cup",{"id":52,"doc_module":4,"doc_module_name":9,"category_name":53,"show_sort_weight":52,"slug":54},10,"Lifestyle","lifestyle",{"id":56,"doc_module":4,"doc_module_name":9,"category_name":57,"show_sort_weight":24,"slug":58},19,"General","general",{"code":4,"msg":60,"data":61},"ok",{"site_id":62,"language":63,"slug":64,"title":65,"keywords":66,"description":67,"schema_data":68,"social_meta":124,"head_meta":126,"extra_data":128,"updated_unix":130},105,"en","aerodynamic-performance-characteristics","Aerodynamic Performance Characteristics","","This document explores aerodynamic performance characteristics, primarily through graphical representations that illustrate key relationships in fluid dynamics. The first image depicts the drag coefficient (CD) plotted against the lift coefficient (CL), showcasing a parabolic approximation of the drag polar. This curve begins with a minimum drag coefficient (CD0) at zero lift and rises as the lift coefficient increases, eventually leading to stall. A critical point highlighted is (L/D)max, representing the maximum lift-to-drag ratio, which occurs at a specific CL value. The second set of graphs presents propeller performance, showing the thrust coefficient (CT) versus the advance ratio (V/nD) for various blade angles. These plots are crucial for understanding propeller efficiency under different operating conditions and are annotated with data points derived from vortex theory. The specific blade angles shown range from 15° to 45°, indicating how variations in angle affect thrust and efficiency across a spectrum of forward speeds. The data suggests that higher blade angles generally produce higher thrust coefficients at lower advance ratios but may lead to reduced efficiency at higher advance ratios. The third, purely black image does not contribute discernible information to the analysis. Overall, the document provides a technical overview of aerodynamic principles and propeller behavior using visual data and theoretical references, essential for aircraft design and performance analysis.",{"@graph":69,"@context":123},[70,84,106],{"@type":71,"itemListElement":72},"BreadcrumbList",[73,77,79,82],{"item":74,"name":75,"@type":76,"position":8},"https://docshare.wps.com","Home","ListItem",{"item":78,"name":9,"@type":76,"position":14},"https://docshare.wps.com/document/",{"item":80,"name":40,"@type":76,"position":81},"https://docshare.wps.com/document/research-report/",3,{"item":83,"name":65,"@type":76,"position":19},"https://docshare.wps.com/document/aerodynamic-performance-characteristics/181296/",{"url":83,"name":65,"@type":85,"image":86,"author":91,"headline":65,"publisher":94,"fileFormat":97,"inLanguage":63,"description":67,"dateModified":98,"datePublished":99,"encodingFormat":97,"isAccessibleForFree":100,"interactionStatistic":101},"DigitalDocument",{"url":87,"@type":88,"width":89,"height":90},"https://docshare.wps.com/thumbnails/aerodynamic-performance-characteristics/181296.png","ImageObject",300,407,{"name":92,"@type":93},"Himbo","Person",{"url":74,"name":95,"@type":96},"DocShare","Organization","application/pdf","2026-10-27","2026-09-02",true,{"@type":102,"interactionType":103,"userInteractionCount":105},"InteractionCounter",{"@type":104},"ViewAction",13,{"@type":107,"mainEntity":108},"FAQPage",[109,115,119],{"name":110,"@type":111,"acceptedAnswer":112},"What does the first graph illustrate?","Question",{"text":113,"@type":114},"The first graph illustrates the relationship between the drag coefficient (CD) and the lift coefficient (CL), showing a parabolic approximation of the drag polar and highlighting the point of maximum lift-to-drag ratio ((L/D)max).","Answer",{"name":116,"@type":111,"acceptedAnswer":117},"What information is presented in the second set of graphs?",{"text":118,"@type":114},"The second set of graphs shows the thrust coefficient (CT) as a function of the advance ratio (V/nD) for different propeller blade angles, indicating how these factors influence propeller performance.",{"name":120,"@type":111,"acceptedAnswer":121},"What is the significance of (L/D)max?",{"text":122,"@type":114},"(L/D)max represents the lift-to-drag ratio at its maximum, which is a crucial point for optimizing aerodynamic efficiency in aircraft design, occurring at a specific lift coefficient value.","https://schema.org",{"og:url":83,"og:type":125,"og:title":65,"og:site_name":95,"og:description":67},"article",{"robots":127,"canonical":83},"index,follow",{"doc_id":129,"site_id":62},181296,1788344115,{"code":4,"msg":5,"data":132},{"doc_id":129,"user_id":133,"nickname":92,"user_avatar":134,"doc_module":4,"category_id":39,"category_name":40,"doc_title":65,"doc_description":67,"doc_content":135,"file_id":136,"file_url":137,"file_type":138,"file_size":139,"view_count":105,"is_deleted":4,"is_public":8,"is_downloadable":8,"audit_status":8,"page_count":52,"language":140,"language_code":63,"site_id":62,"html_lang":63,"table_of_contents":141,"faqs":142,"seo_title":143,"seo_description":67,"update_tm":130,"read_time":144,"preview_page_count":4},687197100911,"https://ap-avatar.wpscdn.com/avatar/a000239b6f1da00475?x-image-process=image/resize,m_fixed,w_180,h_180&k=1785132997149421697","| Paramete\u003Cbr>r | Nilai | Satuan | Sumber |\n| --- | --- | --- | --- |\n| MTOW | 120 | kg | Stenger dkk. 10) |\n| ρFuel | 0,723 | g/cm3 | Sururi dkk.8) |\n| Fuel Rate | 11 / 62 | Lt/min | Muliadi dkk.2)&3) |","cbCaiurN3ZdMFDJL","https://ap.wps.com/l/cbCaiurN3ZdMFDJL","pdf",253072,"English","# Aerodynamic Performance Characteristics\n## Drag Coefficient vs. Lift Coefficient\n## Propeller Performance with Blade Angle","[{\"question\":\"What does the first graph illustrate?\",\"answer\":\"The first graph illustrates the relationship between the drag coefficient (CD) and the lift coefficient (CL), showing a parabolic approximation of the drag polar and highlighting the point of maximum lift-to-drag ratio ((L/D)max).\"},{\"question\":\"What information is presented in the second set of graphs?\",\"answer\":\"The second set of graphs shows the thrust coefficient (CT) as a function of the advance ratio (V/nD) for different propeller blade angles, indicating how these factors influence propeller performance.\"},{\"question\":\"What is the significance of (L/D)max?\",\"answer\":\"(L/D)max represents the lift-to-drag ratio at its maximum, which is a crucial point for optimizing aerodynamic efficiency in aircraft design, occurring at a specific lift coefficient value.\"}]","Aerodynamic Performance Characteristics | PDF",25]