晚来的提名
发表于 2025-3-25 04:19:44
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Gorilla
发表于 2025-3-25 10:02:37
Oleg S. Ryzhov,Elena V. Bogdanova-Ryzhovafully complete their projects. It can help freshly graduated PhDs planning to pursue an academic career, and MDs contemplating a career in research, to decide whether they truly want to embark on this path. Lastly, it can offer young principal investigators a source of inspiration on how to succeed and achieve their goals..978-3-030-85571-0
不愿
发表于 2025-3-25 14:10:03
0926-5112 tage in science alive especially in Gottingen, we were asked by the aerospace research community to organize another symposium. Much had been achieved already i978-94-010-3998-7978-94-010-0017-8Series ISSN 0926-5112 Series E-ISSN 2215-0056
moribund
发表于 2025-3-25 18:28:02
Boundary Layer Instabilities in Transonic Range of Velocities,An extended version of the triple-deck theory is developed for high Mach number subsonic and transonic flows, assuming the Reynolds number to be large enough. The theory embraces unsteady spiral-type Görtier vortices on a concave surface and vortical disturbances in a three-dimensional boundary layer with crossflow on a swept wing or turbine blade.
Callus
发表于 2025-3-25 23:16:06
https://doi.org/10.1007/978-94-010-0017-8aerodynamics; deformation; fluid mechanics; mechanics; oscillation; stress; vibration; wind
contradict
发表于 2025-3-26 01:41:41
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allergy
发表于 2025-3-26 07:24:46
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RLS898
发表于 2025-3-26 11:04:30
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Fraudulent
发表于 2025-3-26 14:16:49
Upstream Propagating Curved Shock in a Steady Transonic Flow,We derive a new set of equations to give successive positions of slowly moving and slowly turning curved shock front in a transonic flow. The equations are in conservation form — two of these are kinematical conservation laws.
神秘
发表于 2025-3-26 19:11:50
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