Computational icing simulations of a hybrid, swept-wing model in the NASA IRT are presented. The results of these simulations are compared to those for the same icing conditions conducted on the full-scale reference wing. The effects of tunnel sidewalls, attachment line position, and altitude are considered. A discussion of icing scaling and the results of one scaling approach are given. The variation of impingement and ice shape with span in the tunnel for different angles of attack and ap deection are presented.
|Original language||English (US)|
|Journal||Transactions of Japanese Society for Medical and Biological Engineering|
|State||Published - Jan 1 2013|
|Event||35th Annual International Conference of IEEE Engineering in Medicine and Biology Society, EMBC 2013 in conjunction with 52nd Annual Conference of Japanese Society for Medical and Bological Engineering, JSMBE - Osaka, Japan|
Duration: Jul 3 2013 → Jul 7 2013
ASJC Scopus subject areas
- Biomedical Engineering