AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |
Back to Blog
Wing clmax from airfoil4/12/2023 But in fact, the pressure P 2 in region 2 is larger than P 1, owing to the compression effect of this moving stage at least P 1= P 2, that is, the number of molecules entering the channel from region 2 is more than region 1. If we let molecular-flow conditions exit within the channel and the pressure P 2 in region 2 be 0, a jet pattern which is disadvantageous for being transmitted by the next stationary stage would be formed at the exit by molecules, most of which have passed through the blade channel without any collision with blade surfaces (refer to Fig. The general parameters are the spacing- chord ratio s/b, the blade angle α, and the ratio of the moving velocity of the blade to the molecular velocity C= u/ Vp. ![]() 3 shows a usual turbo-blade in two dimensions.
0 Comments
Read More
Leave a Reply. |