thrust augmentation 中文意思是什麼
thrust augmentation
解釋
推力增大- thrust : vt （thrust）1 猛推，沖；猛撳，沖入，插入，推入（出），突出，伸出，塞，刺，戳，戳穿。2 逼迫，把[...
- augmentation : n. 1. 擴大，增加。2. 增加物。3. 【音樂】增音。4. 【軍事】擴編。5. 【徽章】名譽副徽。
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The effects of such elements as primary flow total pressure, flow rate, degree of fuel rich, nozzle structure, flying speed and secondary combustion on ejecting mode performance were researched. it was found that thrust augmentation can be achieved on the condition that the flying mach number is above 0. 7. to deeply analyze thrust augmentation mechanism in low speed range, the research was further continued by changing secondary combustion organization and aft - body configuration
研究了一次流總壓、流量、富燃程度、噴管結構、二次流來流速度、二次燃燒組織對引射模態性能的影響，發現實驗樣機構型在0 . 7ma以上的飛行條件下可以獲得推力增強，而在0 . 7ma以下無推力增強。 -
As one of key technologies to acquire the adequate thrust to start the rbcc propulsion system, whether the ejecting technology can produce thrust augmentation in ejecting mode of rbcc is greatly related to whether the potential advantages of rbcc " s high efficiency and low cost can be realized
作為解決rbcc啟動階段動力問題的關鍵技術之一的引射技術能否在rbcc引射模態獲得理想的性能增強關繫到能否真正發揮rbcc大幅度提高航天推進系統經濟性與高效性的潛在優勢。 -
Amount of thrust augmentation
推力增加值 -
It is of great significance to investigate performance characteristics and thrust augmentation mechanism in rbcc engine. this dissertation just deals with the mixing and combustion flow in a experimental strutjet rbcc in ejecting mode to investigate its performance characteristics and thrust augmentation mechanism by applying numerical simulation technique. the detail is as follows : 1
本文應用數值技術對支板式rbcc發動機，即支板火箭引射沖壓組合發動機，引射模態的燃燒與流動現象進行了研究，探討了rbcc引射模態的性能增強機理，主要有以下幾方面： 1
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