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Titlebook: Non-Ideal Compressible Fluid Dynamics for Propulsion and Power; Selected Contributio Francesca di Mare,Andrea Spinelli,Matteo Pini Conferen

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樓主: cobble
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發(fā)表于 2025-3-25 05:00:45 | 只看該作者
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發(fā)表于 2025-3-25 09:57:28 | 只看該作者
Matteo Pini,Carlo De Servinity. A communitarian notion of the self explains how individuals change and develop their identity, or identities, throughout the course of their lifetimes. This can arise commonly as the result of new experiences and the exposure(s) to differing social relationships, education, cultures, religions
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發(fā)表于 2025-3-25 14:24:58 | 只看該作者
ue collection reflecting the past 25 years of Werhane’s work.This volume brings together a selection of papers written by Patricia Werhane during the most recent quarter century. The book critically explicates the direction and development of Werhane’s thinking based on her erudite and eclectic samp
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發(fā)表于 2025-3-25 19:06:37 | 只看該作者
Experimental Investigations of Heat Transfer Processes in Cooling Channels for Cryogenic Hydrogen anial part is the optimal design of the cooling system, with minimal hydrodynamic losses. Therefore a precise knowledge of the heat transfer processes in the combustion chamber and primarily in the cooling channels is necessary. Cooling channels with a high aspect ratio (height-to-width-ratio) in a wa
25#
發(fā)表于 2025-3-25 20:54:05 | 只看該作者
Efficient Handling of Cryogenic Equation of State for the Simulation of Rocket Combustion Chambersand density range. This necessitates the use of more advanced fluid models that impose additional computation overhead. In this study we compare two equation of state (EOS) mixture approximation approaches for cryogenic flows in rocket combustion chambers and present a computationally efficient impl
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發(fā)表于 2025-3-26 01:44:05 | 只看該作者
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發(fā)表于 2025-3-26 04:24:31 | 只看該作者
Pressure-Based Solution Framework for Non-Ideal Flows at All Mach Numbersonfigurations. A cubic equation of state is applied for the accurate description of the thermodynamic state. Different formulations of the pressure equation for sub- and supersonic flows are discussed. The framework is employed to simulate one sub- and one supersonic test case, where experimental da
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發(fā)表于 2025-3-26 09:27:24 | 只看該作者
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發(fā)表于 2025-3-26 14:30:37 | 只看該作者
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