Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges, by T.Dassen (a.o)

Format: Book
Terbitan: , 2000
Online Access: https://webpac.lib.itb.ac.id/search/detail/36651
Daftar Isi:
  • 8 lemb.; gamb., tab., 29 cm.