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樓主: Jaundice
11#
發(fā)表于 2025-3-23 10:02:20 | 只看該作者
Thermal Inverse Design and Optimization, a tool to guide the development of innovative designs of internally cooled, thermally coated or non-coated structures that will cost less to manufacture, have a longer life span, be easier to repair, and sustain higher surface temperatures.
12#
發(fā)表于 2025-3-23 14:53:59 | 只看該作者
13#
發(fā)表于 2025-3-23 19:30:46 | 只看該作者
14#
發(fā)表于 2025-3-24 02:04:36 | 只看該作者
Required Aerodynamic Technologies,lanced contribution of new technologies in all major disciplines is required for realisation of a new Supersonic Commercial Transport (SCT). One of these technologies - usually one of the most important for aircraft-is aerodynamics. Here, the required “pure” aerodynamic technologies are specified in
15#
發(fā)表于 2025-3-24 03:11:53 | 只看該作者
Certification of Supersonic Civil Transports,ndards are to prevent severe accidents in the future which happened in the past (here: after Concorde’s certification). A new SCT has to fulfill these standards, although Concorde had none of these accidents. But accidents - although they sometimes occurred only for a specific aircraft type - have t
16#
發(fā)表于 2025-3-24 08:52:11 | 只看該作者
Gasdynamic Knowledge Base for High Speed Flow Modelling,sonic and supersonic Mach numbers. The purpose is to show the modelling background of a combination of gasdynamics and geometry in the development of modern software for aerodynamic design in the virtual environment of personal and workstation computers. Here it is not intended to once more derive t
17#
發(fā)表于 2025-3-24 11:57:17 | 只看該作者
18#
發(fā)表于 2025-3-24 17:54:00 | 只看該作者
Geometry Generator for CFD and Applied Aerodynamics,ns presented in the two previous book chapters focusing on the interaction between compressible flow with shock waves and flow boundary conditions. The need to have flexible tools for effectively influencing the phenomena occurring in high speed flow calls for development of fast and flexible softwa
19#
發(fā)表于 2025-3-24 19:44:55 | 只看該作者
20#
發(fā)表于 2025-3-25 02:34:20 | 只看該作者
Aerodynamic Shape Optimization Methods,s create configurations that are not optimal even at the design operating conditions [163], [164]. At off design conditions, these configurations often perform quite poorly except when the specified surface pressure distribution, if available at all, would be provided by an extremely accomplished ae
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