{"id":3353,"date":"2024-06-18T13:33:10","date_gmt":"2024-06-18T05:33:10","guid":{"rendered":"https:\/\/cathayvista.top\/?p=3353"},"modified":"2025-01-31T09:51:07","modified_gmt":"2025-01-31T01:51:07","slug":"canard-aeronautics-zhen","status":"publish","type":"post","link":"https:\/\/cathayvista.top\/index.php\/2024\/06\/18\/canard-aeronautics-zhen\/","title":{"rendered":"\u524d\u7ffc\uff08\u9e2d\u7ffc\uff09\/ Canard (aeronautics) &#8211; \u4e2d\u82f1\u6587\u7ef4\u57fa\u767e\u79d1\u8bcd\u6761\u878d\u5408"},"content":{"rendered":"\n<blockquote class=\"wp-block-quote is-layout-flow wp-block-quote-is-layout-flow\">\n<p class=\"has-small-font-size\">\u4e2d\u6587\u8bcd\u6761\u539f\u6587\u94fe\u63a5\uff08\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5185\u5730\u8bbf\u95ee\uff09\uff1a<a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E5%89%8D%E7%BF%BC\" target=\"_blank\" rel=\"noreferrer noopener\">\u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee<\/a> <br>\u82f1\u6587\u8bcd\u6761\u539f\u6587\u94fe\u63a5\uff08\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5185\u5730\u8bbf\u95ee\uff09\uff1a<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)\" target=\"_blank\" rel=\"noreferrer noopener\">\u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee<\/a> <br>\u672c\u6587\u57fa\u4e8e\u82f1\u6587\u8bcd\u6761\u7684\u7ebf\u7d22\uff0c\u5e76\u8865\u5145\u90e8\u5206\u6765\u81ea\u4e2d\u6587\u8bcd\u6761\u7684\u5185\u5bb9\uff08\u5728\u4e8c\u8005\u51b2\u7a81\u65f6\uff0c\u4ee5\u66f4\u665a\u66f4\u65b0\u8005\u4e3a\u51c6\uff09\u3002 \u8fbd\u89c2\u642c\u8fd0\u65f6\u8fdb\u884c\u4e86\u5fc5\u8981\u7684\u5408\u89c4\u5316\u5904\u7406\uff0c\u4ee5\u4f7f\u5176\u80fd\u591f\u5728\u4e2d\u56fd\u5185\u5730\u4e0a\u4f20\u3002 <\/p>\n\n\n\n<p class=\"has-small-font-size\">\u7ef4\u57fa\u767e\u79d1\uff08Wikipedia\uff09\u662f\u7f8e\u56fd\u7ef4\u57fa\u5a92\u4f53\u57fa\u91d1\u4f1a\u7684\u4e92\u8054\u7f51\u767e\u79d1\u9879\u76ee\uff0c\u5176\u5185\u5bb9\u53ef\u80fd\u53d7\u5230\u7acb\u573a\u3001\u4fe1\u606f\u6765\u6e90\u7b49\u56e0\u7d20\u5f71\u54cd\uff0c\u8bf7\u5ba2\u89c2\u770b\u5f85\u3002\u6b63\u6587\u5185\u5bb9\u4e0d\u4ee3\u8868\u8bd1\u8005\u89c2\u70b9\u3002 \u8fbd\u89c2\u63d0\u4f9b\u7684\u7ffb\u8bd1\u4ec5\u4f9b\u53c2\u8003\u3002<\/p>\n\n\n\n<p class=\"has-vivid-red-color has-text-color has-link-color has-small-font-size wp-elements-fa3520ec8a146f3dbaefc7078a38d0d3\">\u6587\u4e2d\u53ef\u80fd\u5305\u542b\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5185\u5730\u8bbf\u95ee\u7684\u94fe\u63a5\u3002 <\/p>\n<cite>\u8fbd\u89c2\u6240\u642c\u8fd0\u7684\u8bcd\u6761\u6587\u672c\u4e0e\u7ef4\u57fa\u767e\u79d1\u4e00\u9053\u540c\u6837\u9075\u5faaCC BY-SA 4.0\u534f\u8bae\uff08<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/653887754?utm_psn=1730141199812366337\" target=\"_blank\" rel=\"noreferrer noopener\">\u8fbd\u89c2\u642c\u8fd0\u7684\u4e2d\u82f1\u6587\u5bf9\u7167\u7248\u672c<\/a>\uff09\uff0c\u5728\u7b26\u5408\u534f\u8bae\u8981\u6c42\u7684\u60c5\u51b5\u4e0b\u60a8\u53ef\u4ee5\u514d\u8d39\u4f7f\u7528\u5176\u5185\u5bb9\uff08\u5305\u62ec\u5546\u7528\uff09\u3002\u56fe\u7247\u548c\u89c6\u9891\u53ef\u80fd\u9075\u5faa\u4e0d\u540c\u7684\u5171\u4eab\u534f\u8bae\u3002<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/666846485?utm_psn=1730141316690960386\" target=\"_blank\" rel=\"noreferrer noopener\">\u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee<\/a><\/cite><\/blockquote>\n\n\n\n<h2 class=\"wp-block-heading\">1. \u6b63\u6587\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u4e13\u680f\uff09<\/h2>\n\n\n\n<p><a href=\"https:\/\/zhuanlan.zhihu.com\/p\/696835937\/\" data-type=\"link\" data-id=\"https:\/\/zhuanlan.zhihu.com\/p\/696835937\/\">\u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee<\/a><\/p>\n\n\n\n<h2 class=\"wp-block-heading\">2. \u53c2\u89c1\uff08\u7ef4\u57fa\u767e\u79d1\u7684\u76f8\u5173\u8bcd\u6761\uff09| See also<\/h2>\n\n\n\n<ul class=\"has-small-font-size wp-block-list\">\n<li><a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E9%A3%9B%E8%A1%8C%E5%8A%9B%E5%AD%B8\">\u98de\u884c\u529b\u5b66<\/a><\/li>\n\n\n\n<li><a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E9%A3%9B%E8%A1%8C%E6%93%8D%E7%B8%B1%E8%A3%9D%E7%BD%AE\">\u98de\u884c\u64cd\u7eb5\u88c5\u7f6e<\/a><\/li>\n\n\n\n<li><a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E6%A9%9F%E7%BF%BC\">\u673a\u7ffc<\/a><\/li>\n\n\n\n<li><a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E7%A9%A9%E5%AE%9A%E6%80%A7\">\u7a33\u5b9a\u6027<\/a><\/li>\n\n\n\n<li><a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E6%B2%99%E6%B4%9B%E7%B6%AD%E9%BE%8D%E5%B1%AC\">\u6c99\u6d1b\u7ef4\u9f99\u5c5e<\/a><\/li>\n\n\n\n<li><a href=\"https:\/\/en.wikipedia.org\/wiki\/List_of_canard_aircraft\">List of canard aircraft<\/a>\u3010\u9e2d\u7ffc\u98de\u673a\u5217\u8868\u3011<\/li>\n\n\n\n<li><a href=\"https:\/\/en.wikipedia.org\/wiki\/Tandem_wing\">Tandem wing<\/a>\u3010\u7eb5\u5217\u673a\u7ffc\u3011<\/li>\n\n\n\n<li><a href=\"https:\/\/en.wikipedia.org\/wiki\/Index_of_aviation_articles\">Index of aviation articles<\/a>\u3010\u822a\u7a7a\u6761\u76ee\u7d22\u5f15\u3011<\/li>\n<\/ul>\n\n\n\n<h2 class=\"wp-block-heading\">3. \u53c2\u8003\u6587\u732e | References<\/h2>\n\n\n\n<h3 class=\"wp-block-heading\">3.1 \u82f1\u6587\u8bcd\u6761\u5f15\u7528\u5217\u8868 | Citations<\/h3>\n\n\n\n<ol class=\"has-small-font-size wp-block-list\">\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-1\">^<\/a><\/strong>\u00a0Wragg, D.;\u00a0<em>Historical Dictionary of Aviation<\/em>, History Press (2008), Page 79.<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-clancy_2-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-clancy_2-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0Clancy, L. J. (1975).\u00a0<em>Aerodynamics<\/em>, Pitman (UK), Halsted (US), 1975. Pages 292-3.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Crane_3-0\">^<\/a><\/strong>\u00a0Crane, Dale (1997),\u00a0<em>Dictionary of Aeronautical Terms<\/em>\u00a0(3rd\u00a0ed.), Aviation Supplies &amp; Academics, p.\u00a086,\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/ISBN_(identifier)\">ISBN<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Special:BookSources\/978-1-56027-287-8\"><bdi>978-1-56027-287-8<\/bdi><\/a>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-4\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/core.ac.uk\/download\/pdf\/36704072.pdf\">Aerodynamic analysis of a canard missile configuration using ANSYS<\/a>\u00a0Calhoun: The NPS Institutional Archive, December 2011. Retrieved 16 June 2021<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-5\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/ntrs.nasa.gov\/api\/citations\/19830019688\/downloads\/19830019688.pdf\">Effect of Tail-Fin Span on Stability and Control Characteristics of a Canard-Controlled Missile at Supersonic Mach Numbers<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/NASA\">NASA<\/a>\u00a0Technical paper 2157, June 1983. Retrieved 16 June 2021<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-6\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/fas.org\/man\/dod-101\/sys\/smart\/lgb.htm\">Laser Guided Bombs<\/a>\u00a0FAS Military Analysis Network, 12 February 2000. Retrieved 16 June 2021<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-c_7-0\">^<\/a><\/strong>\u00a0Villard, Henry Serrano (2002).\u00a0<a href=\"https:\/\/books.google.com\/books?id=tDmR7DhM_uEC&amp;pg=PA40\"><em>Contact!\u00a0: the story of the early aviators<\/em><\/a>. Mineola, NY: Dover Publications. pp.\u00a039\u201353.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/ISBN_(identifier)\">ISBN<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Special:BookSources\/978-0-486-42327-2\"><bdi>978-0-486-42327-2<\/bdi><\/a>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-FOOTNOTEBurns1983_8-0\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#CITEREFBurns1983\">Burns 1983<\/a>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-9\">^<\/a><\/strong>\u00a0Kundu, Ajoy Kumar; Price, Mark A.; Riordan, David (8 April 2019).\u00a0<em>Conceptual Aircraft Design: An Industrial Approach<\/em>. John Wiley and Sons. p.\u00a0237.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-10\">^<\/a><\/strong>\u00a0Culick, F.E.C. (2003).\u00a0<a href=\"http:\/\/authors.library.caltech.edu\/11239\/1\/CULaiaaj03.pdf\">&#8220;The Wright Brothers: First Aeronautical Engineers and Test Pilots&#8221;<\/a>\u00a0(PDF).\u00a0<em>AIAA Journal<\/em>.\u00a0<strong>41<\/strong>\u00a0(6): 985\u20131006.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Bibcode_(identifier)\">Bibcode<\/a>:<a href=\"https:\/\/ui.adsabs.harvard.edu\/abs\/2003AIAAJ..41..985C\">2003AIAAJ..41..985C<\/a>.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/CiteSeerX_(identifier)\">CiteSeerX<\/a>\u00a0<a href=\"https:\/\/citeseerx.ist.psu.edu\/viewdoc\/summary?doi=10.1.1.579.7665\">10.1.1.579.7665<\/a>.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Doi_(identifier)\">doi<\/a>:<a href=\"https:\/\/doi.org\/10.2514%2F2.2046\">10.2514\/2.2046<\/a>. Retrieved\u00a08 August\u00a02015.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-11\">^<\/a><\/strong>\u00a0Jerram, Michael E.\u00a0<em>Incredible Flying Machines<\/em>. Marshall Cavendish, 1980. p.59.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-12\">^<\/a><\/strong>\u00a0<a href=\"http:\/\/www.flightglobal.com\/pdfarchive\/view\/1914\/1914%20-%200286.html\"><em>Flight<\/em><\/a>, Flight global, 14 March 1914, p.\u00a0286.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-13\">^<\/a><\/strong>\u00a0Green, W; Swanborough, G (1994),\u00a0<em>The complete book of fighters<\/em>, Salamander, p.\u00a0163.<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-saab_14-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-saab_14-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-saab_14-2\"><sup><em><strong>c<\/strong><\/em><\/sup><\/a>\u00a0<em>Delta wing canard aircraft<\/em>, US Patent\u00a0<a href=\"https:\/\/patents.google.com\/patent\/US3188022\">US3188022 A<\/a>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-anderson21_15-0\">^<\/a><\/strong>\u00a0Anderson, S.B.;\u00a0<a href=\"https:\/\/ntrs.nasa.gov\/archive\/nasa\/casi.ntrs.nasa.gov\/19870013196.pdf\">A Look at Handling Qualities of Canard Configurations<\/a>, NASA Technical Memorimdum 88354, 1986, page 21.<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-:0_16-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-:0_16-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0Stinton, Daroll,\u00a0<em>The design of the aeroplane<\/em>,\u00a0<q>Rutan canards wrought a change in thinking which might have a profound influence in future<\/q>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-17\">^<\/a><\/strong>\u00a0Anderson, Seth B. (September 1986).\u00a0<a href=\"https:\/\/ntrs.nasa.gov\/archive\/nasa\/casi.ntrs.nasa.gov\/19870013196.pdf\">&#8220;A look at Handling Qualities of Canard Configurations&#8221;<\/a>\u00a0(PDF).\u00a0<em>NASA Technical Memorandum 88354<\/em>: 4\u20135.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-18\">^<\/a><\/strong>\u00a0Pocock, Chris (15 November 2013).\u00a0<a href=\"https:\/\/www.ainonline.com\/aviation-news\/defense\/2013-11-15\/swiss-battle-could-be-euro-canard-turning-point\">&#8220;Swiss Battle Could Be Euro-Canard Turning Point&#8221;<\/a>.\u00a0<em>Aviation International News<\/em>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-19\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/www.flightglobal.com\/jast-hover-tests-to-start-in-june\/15919.article\">&#8220;JAST hover tests to start in June&#8221;<\/a>.\u00a0<em>Flight Global<\/em>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-20\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/aviationweek.com\/defense-space\/aircraft-propulsion\/future-fighter-investment-keeping-eurocanards-competitive\">&#8220;Future Fighter Investment Is Keeping Eurocanards Competitive | Aviation Week Network&#8221;<\/a>.\u00a0<em>aviationweek.com<\/em>.<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Drela_21-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Drela_21-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0Drela, Mark, Aero-astro professor, MIT,\u00a0<a href=\"https:\/\/archive.today\/20130630052932\/http:\/\/www.rcuniverse.com\/forum\/m_3441894\/mpage_2\/printable.htm\"><em>Canard description<\/em><\/a>\u00a0(forum), RC universe, archived from\u00a0<a href=\"http:\/\/www.rcuniverse.com\/forum\/m_3441894\/mpage_2\/printable.htm\">the original<\/a>\u00a0on 30 June 2013.<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Canards_22-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Canards_22-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Canards_22-2\"><sup><em><strong>c<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#CITEREFNeblettMethenyLeifsson2003\">Neblett, Metheny &amp; Leifsson 2003<\/a>.<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-CanardProCon_23-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-CanardProCon_23-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/web.archive.org\/web\/20150503195149\/http:\/\/docs.desktop.aero\/appliedaero\/configuration\/canardProCon.html\"><em>A Summary of Canard Advantages and Disadvantages<\/em><\/a>, Desktop Aero, archived from\u00a0<a href=\"http:\/\/docs.desktop.aero\/appliedaero\/configuration\/canardProCon.html\">the original<\/a>\u00a0on 3 May 2015, retrieved\u00a06 October\u00a02015.<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-raymer1999_24-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-raymer1999_24-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-raymer1999_24-2\"><sup><em><strong>c<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-raymer1999_24-3\"><sup><em><strong>d<\/strong><\/em><\/sup><\/a>\u00a0Raymer, Daniel P. (1999).\u00a0<em>Aircraft Design: A Conceptual Approach<\/em>\u00a0(3\u00a0ed.). AIAA.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/ISBN_(identifier)\">ISBN<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Special:BookSources\/978-1-56347-281-7\"><bdi>978-1-56347-281-7<\/bdi><\/a>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-25\">^<\/a><\/strong>\u00a0Gudmondsson, Snorri (3 September 2013).\u00a0<em>General Aviation Aircraft Design: Applied Methods and Procedures<\/em>. Elsevier Inc.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-26\">^<\/a><\/strong>\u00a0Garrison (2002), page 85; &#8220;the stabilizer in the front&#8230; This is the function of the stabilizer. If it&#8217;s in the back it typically pushes downward, and if it&#8217;s in the front it lifts upward.&#8221;<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-benson-apf_27-0\">^<\/a><\/strong>\u00a0Benson, T (ed.),\u00a0<a href=\"https:\/\/web.archive.org\/web\/20220531090450\/https:\/\/www.grc.nasa.gov\/www\/k-12\/airplane\/airplane.html\">&#8220;Airplane parts and functions&#8221;<\/a>,\u00a0<em>Beginner&#8217;s Guide to Aeronautics<\/em>, NASA Glenn Research Center, archived from\u00a0<a href=\"http:\/\/www.grc.nasa.gov\/WWW\/K-12\/airplane\/airplane.html\">the original<\/a>\u00a0on 31 May 2022, retrieved\u00a030 July\u00a02013,\u00a0<q>On the Wright brother&#8217;s first aircraft, the horizontal stabilizer was placed in front of the wings.<\/q><\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-US6064923A_28-0\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/patents.google.com\/patent\/US6064923\"><em>Aircraft with reduced wing structure loading<\/em><\/a>\u00a0(patent), US, 6064923 A,\u00a0<q>&#8230;a front stabilizer, generally known as a canard stabilizer\u2026<\/q><\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-29\">^<\/a><\/strong>\u00a0<a href=\"http:\/\/www.nasa.gov\/centers\/dryden\/news\/FactSheets\/FS-008-DFRC.html\"><em>X-29<\/em><\/a>\u00a0(fact sheet), Dryden: Nasa, 9 September 2015, FS-008-DFRC,\u00a0<q>The X-29&#8230; while its canards\u2014horizontal stabilizers to control pitch\u2014were in front of the wings instead of on the tail<\/q>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-30\">^<\/a><\/strong>\u00a0Culick,\u00a0<em>AIAA-2001-3385<\/em>,\u00a0<q>Consistently with ignoring the condition of zero net (pitch) moment, the Wrights assumed that in equilibrium the canard carried no load and served only as a control device.<\/q><\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-31\">^<\/a><\/strong>\u00a0Anderson, Seth B (1987). &#8220;A look at handling qualities of canard configurations&#8221;.\u00a0<em>Journal of Guidance, Control, and Dynamics<\/em>.\u00a0<strong>10<\/strong>\u00a0(2): 8.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Bibcode_(identifier)\">Bibcode<\/a>:<a href=\"https:\/\/ui.adsabs.harvard.edu\/abs\/1987JGCD...10..129A\">1987JGCD&#8230;10..129A<\/a>.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Doi_(identifier)\">doi<\/a>:<a href=\"https:\/\/doi.org\/10.2514%2F3.20194\">10.2514\/3.20194<\/a>.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Hdl_(identifier)\">hdl<\/a>:<a href=\"https:\/\/hdl.handle.net\/2060%2F19870013196\">2060\/19870013196<\/a>. TM 88354.\u00a0<q>&#8230;the Flyer was highly unstable&#8230; The lateral\/directional stability and control of the Flyer were marginal<\/q>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-32\">^<\/a><\/strong>\u00a0Garrison (2002), page 85; &#8220;Because the center of gravity is not sitting right on top of the center of lift, but is ahead of it, the aircraft would tip over forard if some balancing force were not provided. This is the function of the stabilizer.&#8221;<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Sherwin_33-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Sherwin_33-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0Sherwin, Keith (1975).\u00a0<em>Man powered flight<\/em>\u00a0(rev reprint\u00a0ed.). Model &amp; Allied Publications. p.\u00a0131.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/ISBN_(identifier)\">ISBN<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Special:BookSources\/978-0-85242-436-0\"><bdi>978-0-85242-436-0<\/bdi><\/a>..<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-34\">^<\/a><\/strong>\u00a0Hoerner, &#8220;Aspect ratio&#8221;,\u00a0<em>Fluid Dynamic Lift<\/em>, pp.\u00a011\u201330.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-35\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/en.wikipedia.org\/w\/index.php?title=Lift-induced_drag&amp;oldid=917751056\">&#8220;Lift-induced drag&#8221;<\/a>,\u00a0<em>Wikipedia<\/em>, 25 September 2019, retrieved\u00a017 March\u00a02020<\/li>\n\n\n\n<li>^\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-ReferenceA_36-0\">Jump up to:<sup><em><strong>a<\/strong><\/em><\/sup><\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-ReferenceA_36-1\"><sup><em><strong>b<\/strong><\/em><\/sup><\/a>\u00a0<em>VariEze Wind Tunnel Investigation<\/em>, Nasa, TP 2382.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-37\">^<\/a><\/strong>\u00a0<em>Tandem aircraft PAT-1<\/em>, Nasa, TM 88354.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-NASA-TM-88354_38-0\">^<\/a><\/strong>\u00a0Anderson, Seth B (1 September 1986),\u00a0<a href=\"https:\/\/ntrs.nasa.gov\/archive\/nasa\/casi.ntrs.nasa.gov\/19870013196_1987013196.pdf\">&#8220;A Look at Handling Qualities of Canard Configurations&#8221;<\/a>\u00a0(PDF),\u00a0<em>Journal of Guidance, Control, and Dynamics<\/em>,\u00a0<strong>10<\/strong>\u00a0(2): 16,\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Bibcode_(identifier)\">Bibcode<\/a>:<a href=\"https:\/\/ui.adsabs.harvard.edu\/abs\/1987JGCD...10..129A\">1987JGCD&#8230;10..129A<\/a>,\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Doi_(identifier)\">doi<\/a>:<a href=\"https:\/\/doi.org\/10.2514%2F3.20194\">10.2514\/3.20194<\/a>,\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Hdl_(identifier)\">hdl<\/a>:<a href=\"https:\/\/hdl.handle.net\/2060%2F19870013196\">2060\/19870013196<\/a>, TM-88354,\u00a0<q>Incorporating roll control on the canard is basically less efficient because of an adverse downwash influence on the main wing opposing the canard rolling-moment input.<\/q><\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Sageaction_39-0\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/web.archive.org\/web\/20150219214246\/http:\/\/sageaction.com\/aircraft_testing1.htm#JetAircraft\">&#8220;Jet Aircraft \u2013 Effect of a close-coupled canard on a swept wing&#8221;<\/a>.\u00a0<em>SAI Research Report<\/em>\u00a0(Abstract). Sage Action. 2009. 7501. Archived from\u00a0<a href=\"http:\/\/www.sageaction.com\/aircraft_testing1.htm#JetAircraft\">the original<\/a>\u00a0on 19 February 2015. Retrieved\u00a025 August\u00a02009.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-40\">^<\/a><\/strong>\u00a0<em>NASA Conference Publication, Issues 2-3<\/em>. Scientific and Technical Information Office, National Aeronautics and Space Administration. 1977. pp.\u00a01\u20132.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-41\">^<\/a><\/strong>\u00a0Probert, B,\u00a0<a href=\"https:\/\/web.archive.org\/web\/20110517202722\/http:\/\/ftp.rta.nato.int\/public\/\"><em>Aspects of Wing Design for Transonic and Supersonic Combat<\/em><\/a>, NATO, archived from\u00a0<a href=\"http:\/\/ftp.rta.nato.int\/public\/\/PubFulltext\/RTO\/EN\/RTO-EN-004\/\/\/$EN-004-19.pdf\">the original<\/a>\u00a0(PDF)\u00a0on 17 May 2011.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-42\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/web.archive.org\/web\/20141127200736\/http:\/\/www.mach-flyg.com\/utg80\/80jas_uc.html\"><em>Aerodynamic highlights of a fourth generation delta canard fighter aircraft<\/em><\/a>, Mach flyg, archived from\u00a0<a href=\"http:\/\/www.mach-flyg.com\/utg80\/80jas_uc.html\">the original<\/a>\u00a0on 27 November 2014.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-43\">^<\/a><\/strong>\u00a0Jones, Lloyd S.;\u00a0<em>U.S. Fighters:\u00a0<\/em>Army &#8211; Air Force 1925 to 1980s<em>, Aero, pp.139-41.<\/em><\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-44\">^<\/a><\/strong>\u00a0Roskam, J (1989),\u00a0<em>Airplane Design: Preliminary Configuration Design and Integration of the Propulsion System<\/em>, Design Analysis &amp; Research, p.\u00a082,\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/ISBN_(identifier)\">ISBN<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Special:BookSources\/978-1-884885-43-3\"><bdi>978-1-884885-43-3<\/bdi><\/a>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-45\">^<\/a><\/strong>\u00a0Group, Techbriefs Media.\u00a0<a href=\"https:\/\/www.techbriefs.com\/component\/content\/article\/tb\/supplements\/mctb\/briefs\/29542\">&#8220;Conformably Stowable Canard&#8221;<\/a>.\u00a0<em>www.techbriefs.com<\/em>. Retrieved\u00a017 March\u00a02020.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-46\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/archive.today\/20120915102903\/http:\/\/www.techbriefs.com\/index.php?option=com_staticxt&amp;staticfile=\/Briefs\/Feb01\/ARC14122.html\"><em>Conformably Stowable Canard<\/em><\/a>\u00a0(tech brief), Ames Research Center, archived from\u00a0<a href=\"http:\/\/www.techbriefs.com\/index.php?option=com_staticxt&amp;staticfile=\/Briefs\/Feb01\/ARC14122.html\">the original<\/a>\u00a0on 15 September 2012.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-47\">^<\/a><\/strong>\u00a0Jones (1974), &#8220;US Bombers&#8221;,\u00a0<em>Aero<\/em>,\u00a0<q>canard vanes<\/q>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-48\">^<\/a><\/strong>\u00a0&#8220;B-1 Roll-out&#8221;,\u00a0<em>Flight<\/em>, 1974,\u00a0<q>canard fins for ride control<\/q>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-49\">^<\/a><\/strong>\u00a0Sweetman, William &#8216;Bill&#8217; (June 1997),\u00a0<a href=\"https:\/\/books.google.com\/books?id=eeWcitAiSBUC&amp;pg=PA104\">&#8220;Top Gun&#8221;<\/a>,\u00a0<em><a href=\"https:\/\/en.wikipedia.org\/wiki\/Popular_Science\">Popular Science<\/a><\/em>: 104.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-50\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/translate.google.com\/translate?u=http%3A%2F%2Feurofighter.airpower.at%2Ffaq.htm&amp;langpair=de%7Cen&amp;hl=en&amp;ie=UTF-8\">&#8220;FAQ Eurofighter (translation).&#8221;<\/a>\u00a0Retrieved 29 November 2009.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-51\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/translate.google.com\/translate?u=http%3A%2F%2Fwww.airpower.at%2Fforum%2Fviewtopic.php%3Ft%3D2629&amp;langpair=de%7Cen&amp;hl=en&amp;ie=UTF-8\">&#8220;Austrian Eurofighter committee of inquiry<\/a>:\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Brigadier\">Brigadier<\/a>\u00a0Dipl.Ing.Knoll about Eurofighter and Stealth, pp. 76\u201377. (English translation)&#8221;\u00a0<em>Google<\/em>. Retrieved 28 November 2009.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-52\">^<\/a><\/strong>\u00a0Sweetman, William &#8216;Bill&#8217; (14 January 2011),\u00a0<a href=\"http:\/\/www.aviationweek.com\/aw\/blogs\/defense\/index.jsp?plckController=Blog&amp;plckScript=blogScript&amp;plckElementId=blogDest&amp;plckBlogPage=BlogViewPost&amp;plckPostId=Blog%3A27ec4a53-dcc8-42d0-bd3a-01329aef79a7Post%3A5c50cb01-bdd0-41cc-b216-fdc89354eb19\">&#8220;From JAST To J-20&#8221;<\/a>,\u00a0<em>Aviation Week<\/em>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-Lockheed_Stealth_53-0\">^<\/a><\/strong>\u00a0Sweetman, William &#8216;Bill&#8217; (2005).\u00a0<a href=\"https:\/\/books.google.com\/books?id=q06Jw1lgcF8C&amp;pg=PA124\"><em>Lockheed Stealth<\/em><\/a>. Zenith Press. pp.\u00a0122\u201324 [124].\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/ISBN_(identifier)\">ISBN<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Special:BookSources\/978-0-7603-1940-6\"><bdi>978-0-7603-1940-6<\/bdi><\/a>.<sup>[<em><a href=\"https:\/\/en.wikipedia.org\/wiki\/Wikipedia:Link_rot\">permanent dead link<\/a><\/em>]<\/sup><\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-54\">^<\/a><\/strong>\u00a0<a href=\"http:\/\/www.designnews.com\/document.asp?doc_id=220162&amp;dfpPParams=ind_182,industry_aero,aid_220162&amp;dfpLayout=article\">&#8220;Agility+Stealth = X-36: formula for an advanced fighter &#8220;<\/a>\u00a0<a href=\"https:\/\/web.archive.org\/web\/20140223001051\/http:\/\/www.designnews.com\/document.asp?doc_id=220162&amp;dfpPParams=ind_182,industry_aero,aid_220162&amp;dfpLayout=article\">Archived<\/a>\u00a02014-02-23 at the\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Wayback_Machine\">Wayback Machine<\/a>\u00a0<em>Design News<\/em>\u00a014 January 2013<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-55\">^<\/a><\/strong>\u00a0Roblin, Sebastien (9 November 2021).\u00a0<a href=\"https:\/\/nationalinterest.org\/blog\/reboot\/how-stealthy-chinas-j-20-fighter-jet-195910\">&#8220;How Stealthy is China&#8217;s J-20 Fighter Jet?&#8221;<\/a>.\u00a0<em>The National Interest<\/em>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-56\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/mikoyanmig29.wixsite.com\/chengdu-j-20\/stealth\">&#8220;Stealth&#8221;<\/a>.\u00a0<em>chengdu-j-20<\/em>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-57\">^<\/a><\/strong>\u00a0<a href=\"https:\/\/airpowerasia.com\/2020\/08\/15\/chengdu-j-20-overhyped-or-reality-a-comprehensive-story\/\">&#8220;Chengdu J-20 Overhyped or Reality \u2013 A Comprehensive Story&#8221;<\/a>. 15 August 2020.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/en.wikipedia.org\/wiki\/Canard_(aeronautics)#cite_ref-58\">^<\/a><\/strong>\u00a0Suciu, Peter.\u00a0<a href=\"https:\/\/www.businessinsider.com\/china-j20-russia-su57-arent-quite-5th-generation-fighter-jets-2023-2\">&#8220;Why China&#8217;s and Russia&#8217;s 5th-generation stealth jets don&#8217;t quite live up to the hype, according to a former US Navy pilot&#8221;<\/a>.\u00a0<em>Business Insider<\/em>.<\/li>\n<\/ol>\n\n\n\n<h3 class=\"wp-block-heading\">3.2 \u82f1\u6587\u8bcd\u6761\u6765\u6e90\u6587\u732e | Bibliography<\/h3>\n\n\n\n<ul class=\"wp-block-list\">\n<li>Burns, BRA (December 1983), &#8220;Were the Wrights Right?&#8221;,\u00a0<em><a href=\"https:\/\/en.wikipedia.org\/wiki\/Air_International\">Air International<\/a><\/em>.<\/li>\n\n\n\n<li>\u2014\u2014\u2014\u2014\u2014 (23 February 1985),\u00a0<a href=\"http:\/\/www.flightglobal.com\/pdfarchive\/view\/1985\/1985%20-%200561.html\">&#8220;Canards: Design with Care&#8221;<\/a>,\u00a0<em><a href=\"https:\/\/en.wikipedia.org\/wiki\/Flight_International\">Flight International<\/a><\/em>, pp.\u00a019\u201321.<\/li>\n\n\n\n<li>Neblett, Evan; Metheny, Michael &#8216;Mike&#8217;; Leifsson, Leifur Thor (17 March 2003),\u00a0<a href=\"https:\/\/web.archive.org\/web\/20080227123111\/http:\/\/www.aoe.vt.edu\/~mason\/Mason_f\/canardsS03.pdf\">&#8220;Canards&#8221;<\/a>\u00a0(PDF),\u00a0<em>AOE 4124 Class notes<\/em>, Department of Aerospace and Ocean Engineering, Virginia Tech, archived from\u00a0<a href=\"http:\/\/www.aoe.vt.edu\/~mason\/Mason_f\/canardsS03.pdf\">the original<\/a>\u00a0(PDF)\u00a0on 27 February 2008.<\/li>\n\n\n\n<li>Garrison, P (December 2002),\u00a0<a href=\"https:\/\/books.google.com\/books?id=kZcn7cMVfZcC&amp;q=canard+stabilizer&amp;pg=PA85\">&#8220;Three&#8217;s Company&#8221;<\/a>,\u00a0<em><a href=\"https:\/\/en.wikipedia.org\/wiki\/Flying_(magazine)\">Flying<\/a><\/em>, vol.\u00a0129, no.\u00a012, pp.\u00a085\u201386<\/li>\n\n\n\n<li>Raymer, Daniel P. (1992).\u00a0<a href=\"https:\/\/archive.org\/details\/aircraftdesignco0000raym\"><em>Aircraft Design: A Conceptual Approach<\/em><\/a>\u00a0(2nd\u00a0ed.). Washington:\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/AIAA\">AIAA<\/a>.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/ISBN_(identifier)\">ISBN<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Special:BookSources\/9780930403515\"><bdi>9780930403515<\/bdi><\/a>.\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/OCLC_(identifier)\">OCLC<\/a>\u00a0<a href=\"https:\/\/www.worldcat.org\/oclc\/0930403517\">0930403517<\/a>.<\/li>\n<\/ul>\n\n\n\n<h3 class=\"wp-block-heading\">3.3 \u4e2d\u6587\u8bcd\u6761<\/h3>\n\n\n\n<ol class=\"has-small-font-size wp-block-list\">\n<li>^\u00a0<a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E5%89%8D%E7%BF%BC#cite_ref-iof_1-0\">\u8df3\u8f6c\u5230\uff1a<sup><strong>1.0<\/strong><\/sup><\/a>\u00a0<a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E5%89%8D%E7%BF%BC#cite_ref-iof_1-1\"><sup><strong>1.1<\/strong><\/sup><\/a>\u00a0Jonh Anderson. Introduce to Flight\uff0c5th. ed.. New York: McGRAW-Hill. 2005.\u00a0<a href=\"https:\/\/zh.wikipedia.org\/wiki\/Special:%E7%BD%91%E7%BB%9C%E4%B9%A6%E6%BA%90\/0071238182\">ISBN\u00a00071238182<\/a>.<\/li>\n\n\n\n<li><strong><a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E5%89%8D%E7%BF%BC#cite_ref-2\">^<\/a><\/strong>\u00a0Warren Phillips.\u00a0<a href=\"https:\/\/archive.org\/details\/mechanicsoffligh0000phil\">Mechanics of Flight<\/a>. Hoboken: Wiley. 2004.\u00a0<a href=\"https:\/\/zh.wikipedia.org\/wiki\/Special:%E7%BD%91%E7%BB%9C%E4%B9%A6%E6%BA%90\/0471334588\">ISBN\u00a00471334588<\/a>.<\/li>\n<\/ol>\n\n\n\n<h2 class=\"wp-block-heading\">4. \u5ef6\u4f38\u9605\u8bfb | Further reading<\/h2>\n\n\n\n<ul class=\"has-small-font-size wp-block-list\">\n<li>Abzug; Larrabee (2002),\u00a0<em>Airplane Stability and Control<\/em>, Cambridge University Press,\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/ISBN_(identifier)\">ISBN<\/a>\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/Special:BookSources\/9781107321427\"><bdi>9781107321427<\/bdi><\/a>,\u00a0<a href=\"https:\/\/en.wikipedia.org\/wiki\/OCLC_(identifier)\">OCLC<\/a>\u00a0<a href=\"https:\/\/www.worldcat.org\/oclc\/829704722\">829704722<\/a>.<\/li>\n\n\n\n<li>Gambu, J; Perard, J (January 1973), &#8220;Saab 37 Viggen&#8221;,\u00a0<em>Aviation International<\/em>, no.\u00a0602, pp.\u00a029\u201340.<\/li>\n\n\n\n<li>Lennon, Andy (1984),\u00a0<em>Canard\u00a0: a revolution in flight<\/em>, Aviation.<\/li>\n\n\n\n<li>Rollo, Vera Foster (1991),\u00a0<em>Burt Rutan Reinventing the Airplane<\/em>, Maryland Historical Press.<\/li>\n\n\n\n<li>Wilkinson, R (2001).\u00a0<em>Aircraft Structures and Systems<\/em>\u00a0(2nd\u00a0ed.). MechAero Publishing.<\/li>\n\n\n\n<li>Selberg, Bruce P; Cronin, Donald L,\u00a0<em>Aerodynamic-Structural Study of Canard Wing, Dual Wing, and Conventional Wing Systems for General Aviation Applications. University of Missouri-Rolla. Contract Report 172529<\/em>, National Aeronautics and Space Administration\u00a0<a href=\"https:\/\/ntrs.nasa.gov\/archive\/nasa\/casi.ntrs.nasa.gov\/19850008520.pdf\">Aerodynamic-structural study of canard wing, dual wing, and conventional wing systems for general aviation applications<\/a><\/li>\n<\/ul>\n\n\n\n<h2 class=\"wp-block-heading\">5. \u5916\u90e8\u94fe\u63a5 | External links<\/h2>\n\n\n\n<p>Wikimedia Commons has media related to\u00a0<strong><em><a href=\"https:\/\/commons.wikimedia.org\/wiki\/Category:Canard_wings\">Canard wings<\/a><\/em><\/strong>.\u3010\u7ef4\u57fa\u5171\u4eab\u8d44\u6e90\u4e2d\u62e5\u6709\u4e0e\u9e2d\u7ffc\u76f8\u5173\u7684\u5a92\u4f53\u3002\u3011<\/p>\n","protected":false},"excerpt":{"rendered":"<p>\u4e2d\u6587\u8bcd\u6761\u539f\u6587\u94fe\u63a5\uff08\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5185\u5730\u8bbf\u95ee\uff09\uff1a\u8bf7\u70b9 [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":[],"categories":[21],"tags":[155,101],"class_list":["post-3353","post","type-post","status-publish","format-standard","hentry","category-aviation","tag-155","tag-101"],"_links":{"self":[{"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/posts\/3353","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/comments?post=3353"}],"version-history":[{"count":0,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/posts\/3353\/revisions"}],"wp:attachment":[{"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/media?parent=3353"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/categories?post=3353"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/tags?post=3353"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}