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Development and Validation of Numerical Methods for Transonic / Low Supersonic Microflow Devices at ESTEC

机译：ESTEC跨音速/低超音速微流装置数值方法的开发和验证

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《AIAA Aerospace Sciences Meeting and Exhibit》|2005年|P.1-8|共8页
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B. Thornber; R. Schwane; O. Gloth;
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中图分类航空;
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3. Flow Around a Conical Nose with Rounded Tail Projectile for Subsonic, Transonic, and Supersonic Flow Regimes : A Numerical Study [J] . Amitesh Kumar, H. S. Panda, T. K. Biswal, Defence science journal . 2014,第6期

机译：亚音速，跨音速和超音速流态的带有圆尾弹头的锥形鼻孔流场：数值研究
4. Development and Validation of Numerical Methods for Transonic / Low Supersonic Microflow Devices at ESTEC [C] . American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting and Exhibit . 2005

机译：eSTEC跨型/低超音速微流量器件数值方法的开发与验证
5. High-resolution TVD schemes for the analysis of: I. Inviscid supersonic and transonic flows. II. Viscous flows with shock-induced separation and heat transfer. [D] . Driver, Mark Anthony. 1991

机译：用于分析以下内容的高分辨率TVD方案：I.超音速和跨音速无粘性流。二。粘性流具有激振引起的分离和热传递。
6. Efficient supersonic flow simulations using lattice Boltzmann methods based on numerical equilibria [O] . Jonas Latt, Christophe Coreixas, Joël Beny, -1

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7. Numerical flow simulation methods and additive manufacturing methods for the development of a flow optimised design of a novel point-of-care diagnostic device [O] . Dethloff Manuel, Seitz Hermann, Dangers Marc 2017

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8. Studies in Transonic, Supersonic, and Separated Flows Using Numerical Methods [R] . Holt, M. 1976

机译：使用数值方法研究跨音速，超音速和分离流动

Development and Validation of Numerical Methods for Transonic / Low Supersonic Microflow Devices at ESTEC

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