The Shenyang J-13 (Chinese: 歼-13; traditional: 殲-13) was a long-running Chinese project by Shenyang Aircraft Corporation to develop a light-weight, single engine fighter aircraft, which was ultimately cancelled. [1]

J--13 adopts single-engine abdomen air intake layout. Since the air inlet is below the fuselage and is not the main bearing structure, it hinders the layout of the landing gear. The sinking rate of...

2020年3月14日 · 歼13方案落败的核心原因，包括其功能设计非常简陋，性能指标和应用技术过于落后；它被定位在一种低功能的白昼近距格斗飞机，不具备超视距和全天候作战能力；而其机动性又并不理想，理论上比歼7和歼8要好点，但根本不足以和F16等真正的三代机相提并论。

First, as an absolute air superiority fighter, the J-13 needs to have the largest possible Mach number as possible to pursue or evade enemy aircraft, and also needs to be able to fly at subsonic...

2016年11月11日 · Service introduction of this aircraft came in 2005 with some 400 having been built since (2016). The finalized J-13 was to feature a slim fuselage with mid-set wing mainplanes. The mainplanes were given straight trailing edges and swept leading edges, meeting a short section of wing root at the fuselage sides.

歼-13（中国编号：J-13，英文：CAC J-13）战斗机，是中国20世纪70年代初提出的战斗机设计方案。 [1] 百度百科是一部内容开放、自由的网络百科全书，旨在创造一个涵盖所有领域知识，服务所有互联网用户的中文知识性百科全书。 在这里你可以参与词条编辑，分享贡献你的知识。

2022年7月21日 · 歼-13（中国编号：J-13，英文：CAC J-13）战斗机，是中国20世纪70年代初提出的战斗机设计方案。 中国海军20世纪80年代曾提出舰载机设想，据此601所提出歼-13改舰载机方案。 歼-13采用单发机腹进气布局，由于进气道在机身下面并且不是主承力结构，妨碍了起落架的布置，舰载机的下沉率比岸基飞机要大的多，所以机腹进气飞机的改装舰载机存在较大困难。

The Shenyang J-13 (Chinese: 歼-13; traditional: 殲-13) is a light-weight, single engine fighter aircraft in service in the People's Liberation Army Air Force from 1992 onwards.

Estimated specs include a top speed of Mach 2.45, a combat radius of 2,3450km and a service cap of up to 19,000m. 1 x Woshan WS-6 or WP-15 turbofan engine producing at least 26,455 lbs of thrust after afterburning.

The J-13 was to be a single-engine, single-seat, light-weight, indigenously developed, air-superiority fighter. The J-13's finalised design was a cantilever winged fighter with fuselage side mounted air intakes.