Document is current

Any future updates will be listed below

Analysis of Damping Derivatives for Delta Wings in Hypersonic Flow for Curved Leading Edges with Full Sine Wave

Crossref DOI link: https://doi.org/10.35940/ijeat.A3086.109119

Published Online: 2019-10-30

Update policy: https://doi.org/10.35940/beiesp.crossmarkpolicy

About CrossMark