Three-dimensional flow structure along simultaneously pitching and rotating wings: effect of pitch rate
Crossref DOI link: https://doi.org/10.1007/s00348-015-1952-4
Published Online: 2015-04-08
Published Print: 2015-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Bross, M.
Rockwell, D.
Funding for this research was provided by:
Air Force Office of Scientific Research (FA9550-11-1-0069)
Text and Data Mining valid from 2015-04-01
Version of Record valid from 2015-04-01
Article History
Received: 8 December 2014
Revised: 20 March 2015
Accepted: 30 March 2015
First Online: 8 April 2015