steady acceleration 中文意思是什麼
steady acceleration
解釋
等加速度- steady : adj 1 穩固的，平穩的，穩定的，不變的（腳步、努力等）。2 堅定的，扎實的，牢靠的（船等）。3 有規則...
- acceleration : n. 1. 加速；促進。2. 【物理學】加速度；變速。3. 【教育】加速升級。
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The viscid flux is discretized by second - order central difference scheme. baldwin - lomax turbulence model is implemented in navier - stokes flow solver. for steady - state calculations, a four - stage runge - kutta scheme with convergence acceleration techniques such as local - time stepping and implicit residual smoothing is used
其中，定常計算中的時間推進採用四步runge ? kutta方法，並應用了當地時間步長、隱式殘值光順等加速收斂措施；非定常計算中的時間推進採用jameson的隱式雙時間方法。 -
Optics and optical instruments - environmental test methods - combined bounce or steady state acceleration, in dry heat or cold
彈跳或恆加速度與高溫低溫綜合試驗 -
Environmental tests for aircraft equipment - steady - state acceleration
飛行器的環境試驗.穩態加速 -
Optics and optical instruments - environmental test methods - combined bounce or steady - state acceleration and dry heat or cold
光學和光學儀器.環境試驗方法.混合式跳動或穩態加速度與乾熱或乾冷 -
Optics and optical instruments - environmental test methods - part 16 : combined bounce or steady - state acceleration and dry heat or cold iso 9022 - 16 : 1998
光學和光學儀器.環境試驗方法.第16部分:跳動或穩定狀 -
Ea environmental testing for electric and electronic products. part 2 : test methods. mounting of components, equipment and other articles for dynamic tests including shock, bump, vibration fc and fd and steady - state acceleration and guidance
電工電子產品環境試驗第2部分:試驗方法元件設備和其他產品在沖擊 -
This experiential formula can be used in simulating steady condition, startup, acceleration work process and integrated design of cruise missile and turbofan engine so as to improve the accuracy of 1d engine performance computation
該經驗公式可用於彈用發動機穩態、起動、加速過程的計算和導彈與發動機一體化設計的數值模擬模型，從而提高發動機性能數值模擬的準確性。 -
The analysis is focused on the acceleration influence on burn rate of the grain when the solid rocket motor is working under lateral overload. the simple model of burn rate in acceleration field is established. moving laws of burn surface for two different grain type srms are respectively derived, on the base of which zero dimension and one dimension quasi - steady internal ballistic simulation models are established
分析了橫向過載對固體推進劑燃速的影響，建立了橫向加速度場中的簡化燃速模型，推導了兩種不同藥型的燃面退移規律，在此基礎上進行了零維、一維準定常內彈道計算與分析，建立了固體火箭發動機內流場三維兩相流模型。
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