Experimental study of two electro-mechanical de-icing systems applied on a wing section tested in an icing wind tunnel
Year: 2017
Type: article
Source: CEAS Aeronautical Journal
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Helmholtz-Gemeinschaft
OpenAlex ID: W2554920324
