本帖最后由 choi 于 10-29-2018 15:32 编辑
朱明, 【獨家】雲峰中程飛彈2019年量產 機動部署北、中部約20枚直攻北京. 上報 UP Media, Oct 29, 2018.
https://www.upmedia.mg/news_info.php?SerialNo=50887
("射程超過1200公里的「雲峰中程飛彈」2019年啟動量產計劃")
Note: "中科院研發的雲峰中程飛彈 * * * 先由4個天弓彈體的固體燃料火箭點燃將雲峰飛彈推進到一定高度後,這4個天弓彈體推進器脫落後,主彈體的沖壓引擎,被歸類為中程陸攻衝壓飛彈,也是高空高速巡弋飛彈 [cruise, not ballistic, missile; BALLISTIC missile classification by range: 'medium-range ballistic missile (MRBM): Range between 1,000 km and 3,500 km': Wikipedia],並不在《國際反彈道飛彈擴散條約》(MTCR)的規範內。"
(a) 衝壓發動機 (cn.wikipedia.org)/ 沖壓引擎 (this report) ramjet.
(i) Firstly, a review of turbojet
https://en.wikipedia.org/wiki/Turbojet
There is no need to read the rest. Go to section 3, section 3.2 Compressor + section 3.3 combustion chamber. To the right of each is an animation:
• "An animation of an axial compressor. The stationary blades are the stators." Pay attention to sentence 1 in this quotation.
• "Turbojet animation" (where the compressor is represented by a single ring, as opposed to multiple rings, of rotating blades)
For a decade, I could not figure out whether the thrust came from compressor or combustion. Today I learn the answer is mostly, but altogether -- the latter -- (see (a)(iv) below) ), the energy released from fuel combustion (as in gas-engine car; fuel is packed with energy).
(ii) Ramjet has no compressor, hence the need for propulsion by other means ("先由4個天弓彈體的固體燃料火箭點燃將雲峰飛彈推進") to reach supersonic velocity (say, Mach 3; maximal velocity for ramjet is Mach 6; en.wikipedia.org for ramjet). At that velocity, air comes into the ramjet automatically, combustion thrust ramjet forward, and "a ramjet will be self-sustaining." Id. That same Wiki page states in section 10 Missiles using ramjets: India, Russia and Taiwan (Hsiung Feng or Brave Wind III 雄風三型 which is anti-ship) have, but not US, Britain or China (US and Britain had them before). There is no need to read the rest of this Wiki page.
(iii) Ramjet Parts. NASA, undated
https://www.grc.nasa.gov/www/k-12/airplane/rampart.html
, which is deceptively simple (but hardwork is required to iron out the kinks).
(iv) Fred Landis, Jet Propulsion. Compton's Interactive Encyclopedia, date unknown.
www.fem.unicamp.br/~em313/paginas/consulte/jet.htm
(remarks for both turbojet and ramjet)
(A) In the URL, FEM is an acronym of Faculdade de Engenharia Mecânica, Portuguese for "School of Mechanical Engineering," and Unicamp is short for "University of Campinas" (1962- ; public; Location Campinas, São Paulo, Brazil) en.wikipedia.org.
https://en.wikipedia.org/wiki/University_of_Campinas
(B) Compton's Encyclopedia ( was founded by Frank E Compton in 1922; sold and current publisher is Encyclopedia Britannica) Wikipedia.
(C) Centrifugal Compressor: Principle, Construction, Working, Types, Advantages, Disadvantages with its Application. Mech4study.com, Nov 14, 2017
www.mech4study.com/2017/11/centrifugal-compressor.html
View top graphic only: Take notice that "suction side" and "discharge side" are in different directions -- a hallmark of centrifugal compressor:
(D) Axial compressor "is a rotating, airfoil-based compressor in which the gas or working fluid principally flows parallel to the axis of rotation, or axially." n.wikipedia.org for axial compressor.
(E) Turbojet engine has moving parts, but "moving parts will damage at high velocity." from the Web. That is why ramjet does not have moving parts.
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