adj.空氣熱力學(xué)的

The comparison between the gas models appeared great difference for both aerodynamic and aerothermodynamic. 第三，通過數(shù)值試驗，分析了氣體模型和溫度模型對熱流的影響，對于來流焓值較低的流動，在馬赫數(shù)較小的情況下，溫度升高并不明顯，完全氣體模型仍然使用，但是對于高焓值以及較大馬赫數(shù)的流動，溫度升高很多，完全氣體模型不再適用，必須采用不同的氣體模型來代替，本文中采用化學(xué)非平衡氣體模型。

Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine. 摘要為了使氣動熱力模型更好的逼近渦輪發(fā)動機(jī)，應(yīng)用成熟的非均勻B樣條來擬合部件特性。

In accordance with large temperature gradient in multi-stage turbine channel,an aerothermodynamic method is proposed for varying specific heat solution of S 2 surface to consider precisely the effect of temperature variation on the computed results. 針對在多級渦輪流道中沿流動方向燃?xì)鉁囟茸兓^大這一特點(diǎn)，為了準(zhǔn)確反映出溫度變化對氣動熱力計算結(jié)果的影響，提出了一種考慮變比熱影響的S2流面的氣動熱力計算方法。

Some Aerothermodynamic Aspects of ESA Entry Probes ESA再入探測器的某些空氣熱動力問題(英文)

Aerothermodynamic Elastic Vehicle 氣動熱力彈性器

n.空氣熱力學(xué)