Investigation into the flow behaviour of a NACA 0021 airfoil with leading edge undulations simulated with RANS in STAR-CCM+

Kevin Atkins

Research output: ThesisMaster's Thesis

1925 Downloads (Pure)
Original languageEnglish
Awarding Institution
  • University of Manchester
Place of PublicationManchester, UK
Publisher
Publication statusPublished - Sept 2015

Cite this