Hypersonic boundary-layer separation detection with pressure-sensitive paint for a cone at high angle of attack
Crossref DOI link: https://doi.org/10.1007/s00348-018-2665-2
Published Online: 2019-01-03
Published Print: 2019-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Running, Carson L.
Sakaue, Hirotaka
Juliano, Thomas J.
Text and Data Mining valid from 2019-01-01
Article History
Received: 1 June 2018
Revised: 6 December 2018
Accepted: 13 December 2018
First Online: 3 January 2019