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Showing 1 to 2 of 2 for “"GRCop"”.

  1. Structural Optimization of Regeneratively Cooled Rotating Detonation Rocket Engines

    … rate for several candidate combustor materials – GRCop-84, IN718, W-25Re, Nb-C103. The deviatoric stress in the hot wall increases monotonically with propellant flow rate. In all cases onset of yielding limits the maximum achievable flow rate. W-25Re can achieve the highest propellant flow rate of …

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  2. Design and development of Cu-based alloys for AM in the aerospace context

    L'abstract è presente nell'allegato / the abstract is in the attachment

    poli-torino Repository record for Design and development of Cu-based alloys for AM in the aerospace context (opens in a new tab)