paragon
发表于 2025-3-25 07:05:20
Investigation of the Impact of Simplifying the Aircraft Geometry on the Characteristics of the Verthe influence of simplifying the aircraft geometry on the characteristics of the VTP is examined. Four different configurations with varying simplification level were investigated. These are: a VTP on a base plate, a VTP on a fuselage, a VTP on a fuselage with horizontal tailplane and a VTP on a fuse
dura-mater
发表于 2025-3-25 09:00:09
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彻底检查
发表于 2025-3-25 13:49:08
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推崇
发表于 2025-3-25 16:54:05
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rectum
发表于 2025-3-25 22:32:28
Analytical Design of an Inlet Distortion Generator and Its Experimental and Numerical Validation,homogeneous flow to the fan in a compressor rig’s inlet is meant to be disturbed by specifically modeled inlet separations in order to investigate the impact of distortion on the performance of the compressor. Therefore a suitable distortion generator was designed analytically and validated experime
青春期
发表于 2025-3-26 03:49:53
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abject
发表于 2025-3-26 07:53:50
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寄生虫
发表于 2025-3-26 10:49:56
Development of the Adjoint Approach for Aeroelastic Wing Optimization, of the cost function with respect to the design variables; also called the sensitivities. The traditional approach to calculate the sensitivities, the finite differences, can become prohibitively expensive in high-fidelity optimizations context. For this reason an existing flow adjoint approach was
ellagic-acid
发表于 2025-3-26 13:34:53
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Tailor
发表于 2025-3-26 17:11:14
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