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- Demand Mode Integral Rocket Ramjet 指令型整體式火箭沖壓噴氣發(fā)動(dòng)機
- Integral Rocket Ramjet Surface-to Surface Missile 集裝沖壓式火箭發(fā)動(dòng)機地對地導彈
- Integral Rocket Ramjet Surface-to-Air Missile 集裝沖壓式火箭發(fā)動(dòng)機地(水面)對空導彈
- Integral Rocket Ramjet Torpedo Tube Missile 集裝沖壓式火箭發(fā)動(dòng)機魚(yú)雷發(fā)射管導彈
- Keywords Integral rocket ramjet;Ducted rocket engine;Flow control;Oxygen poor fuel rich propellant; 整體式火箭沖壓發(fā)動(dòng)機;沖壓火箭發(fā)動(dòng)機;流量控制;貧氧富燃料推進(jìn)劑;
- Integrated Rocket Ramjet Component Integration Study 火箭沖壓發(fā)動(dòng)機機件組合研究
- Integral rocket ramjet 整體式火箭沖壓發(fā)動(dòng)機
- This paper established the mathematical models of integral solid rocket ramjet, aerodynamics and trajectory, and wrote the corresponding C++ code. 本文建立了固體火箭沖壓發(fā)動(dòng)機性能計算、導彈氣動(dòng)性能計算和彈道仿真分析等分系統的數學(xué)模型，并編制了相應的C++計算程序模塊。
- The secondary combustion of full-scale solid rocket ramjet was investigated by using the ground direct-connected experimental equipment with uncertainty evaluation. 采用不確定度評定的地面直連沖壓實(shí)驗設備,對某全尺寸固沖發(fā)動(dòng)機補燃室二次燃燒進(jìn)行了實(shí)驗研究。
- The numerical simulation of supersonic inlet internal turbulent flow of solid rocket ramjet assisted range projectiles was performed by 2-order implicit TVD. 摘要應用二階隱式TVD格式對固體火箭沖壓發(fā)動(dòng)機增程彈丸超音速進(jìn)氣道內部湍流流場(chǎng)進(jìn)行了數值仿真。
- In addition, the USAF continues to fund development work of the Aerojet (formerly Atlantic Research) Variable Flow Ducted Rocket ramjet system as a future propulsion option for an extended range AAM. 此外，美國空軍繼續投資于航空噴氣研究所（原來(lái)的大西洋研究所）的可變噴流管火箭發(fā)動(dòng)機系統，將其作為增程空空導彈的未來(lái)推進(jìn)選項。
- With zonal patched grid technology and second-order zonal solver method, the numerical simulation on inlet complex flow field of solid rocket ramjet assisted range projectiles with different struts shapes was made at different Mach numbers. 摘要結合分區對接網(wǎng)格技術(shù)和二階精度區域分解算法，對某沖壓增程彈丸進(jìn)氣道在不同來(lái)流攻角和不同側向支柱形狀工況下的內外復雜流場(chǎng)進(jìn)行了數值模擬。
- An Application Research of Integral Sol id Propellant Rocket Ramjets 整體式固體火箭沖壓發(fā)動(dòng)機的應用性能探討
- Gas Flow Control Technique of Rocket Ramjet 固體火箭沖壓發(fā)動(dòng)機燃氣流量調節技術(shù)與實(shí)驗研究
- Advanced Surface to Air Rocket Ramjet 新型地(水面)對空火箭沖壓式噴氣發(fā)動(dòng)機
- Our pilotless rocket enters the track of the earth. 我們把一個(gè)無(wú)人駕駛的火箭送入了地球的軌道里。
- Genetic algorithm applied to integral design optimization of missile propelled by solid rocket ramjet 固體火箭沖壓發(fā)動(dòng)機導彈一體化遺傳算法優(yōu)化設計
- The kitchen is an integral part of a house. 廚房是房子不可缺的部分
- They planned to send a rocket to the moon. 他們計劃向月球發(fā)射火箭。
- Multimethod Collaborative Optimization Algorithm Applied to Integral Optimal Design of Missile Propelled by Unchoked Solid Rocket Ramjet 基于多方法協(xié)作優(yōu)化方法的非壅塞式固體火箭沖壓發(fā)動(dòng)機導彈一體化優(yōu)化設計
