plane shock 中文意思是什麼
plane shock
解釋
平面沖波-
With account for the effect of temperature and shock - boundary layer interaction, the forebody / inlet with plane lip and wedge lip are designed by using the design methods of constant shock wave intensity and constant shock wave angle. in the design, the incidence angle of the first ramp, height of isolator, length of forebody and total turning angle of the designed forebody / inlet models are given
另外，根據優選結果，給定前體長度、前體預壓縮楔角、總壓縮轉角及隔離段高度，分別用等激波強度和等激波角度的方法設計了唇口平直和唇口帶楔角的前體進氣道。 -
The calculation results indicate that the starting performance of forebody / inlet with wedge - shaped lip is better than that with plane lip at low flight mach number. at high flight mach number, the performance of the forebody / inlets designed by the two methods is approximate. at low flight mach number, the starting performance of forebody / inlet designed by the method of constant shock wave intensity is better
結果表明：唇口帶楔角的進氣道在低飛行馬赫數下的起動性能優于唇口平直的進氣道；採用等激波強度和等激波角度方法設計的進氣道在高飛行馬赫數下的性能相近，在低飛行馬赫數下，採用等激波強度方法設計的進氣道起動性能較優。 -
The strike - slip faulting was caused by asymmetrical distribution of barriers on the subducting plate. the nne - ssw distributed aftershocks occurred on, or near, the fault plane of the main shock ; while the nw - se distributed aftershocks, on, or near, the mentawai fault
北北東?南南西向分佈的餘震發生在主震的斷層面上（或其附近） ；而西北?東南向分佈的餘震則發生在明打威斷層上（或其附近） 。 -
The double shock pair is nearly symmetrical with respect to the central normal of the disturbance source in the heliospheric meridional plane, whereas it is asymmetrical in the heliospheric equatorial plane
該4個激波按離太陽由近及遠依次為後向快激波、後向慢激波、前向慢激波和前向快激波。 -
Meanwhile the 0 dimension 1 dimension plane wall 2 dimension models are established. using the mathematic and ansys software the numerical and soluble analyses can be got for the thermal shock model of the piston. compare the simulation results to the test results the temperature field and stress field can be got which are quite close the thermal shock situation
同時建立活塞熱沖擊的集總參數、 1維平壁和2維模型，應用mathematic軟體和ansys軟體，對所建立的活塞熱沖擊模型進行了解析和數值分析，利用模擬計算與試驗結果相結合的方法，獲得接近於內燃機活塞熱沖擊的溫度場與熱應力場分佈，從而更加全面深入地了解在熱沖擊條件下活塞的溫度場和應力場變化規律。 -
Formation process of cavitation region effected by underwater plane blast shock wave and its characteristics
水下平面爆炸沖擊作用下空化區域形成及其特徵 -
In addition, by phase plane method we obtain the existence of travelling fronts ( al ) connecting two adjacent equilibria under the assumptions that f " is bounded and that of viscous shock waves c connecting two adjacent saddle points with / a convex function
另外，利用經典的相平面分析法，本文證明了（ ）在f有界時存在連接相鄰平衡點的波前（ a1 ）及在f為凸時存在連接相鄰鞍點的粘性沖擊波c 。 -
On the western side of the central normal of the disturbance source in the heliospheric equatorial plane, the double shock pair structure is more evident, and the longitudinal span is wider than those on the eastern side
雙重激波對在子午面內相對擾動源中心法線基本對稱，而在赤道面內則不對稱：擾動源中心法線西側雙重激波對結構更為明顯，所跨經度范圍寬于東側。 -
3. the random theory is applied to the thermal shock model in the first time. the lumped parameter system and the plane wall random model have been established and the simulated results are also have been got
其原理完全適用於計算3維有限元活塞隨機溫度或採用其它數值方法（差分法、離散化法、邊界元法、 … … ）計算隨機溫度場。
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