# Optimization and design of an aircraft's morphing wing-tip demonstrator for drag reduction at low speeds, Part II - Experimental validation using Infra-Red transition measurement from Wind Tunnel tests

> Research article (Chinese Journal of Aeronautics, 2017) · cited 57× · AI/ML

**Wikidata**: [openalex:W2571372758](https://www.wikidata.org/wiki/openalex:W2571372758)  
**Source**: https://4ort.xyz/entity/optimization-and-design-of-an-aircraft-s-morphing-wing-tip-demonstrator-for-drag-reduction-at-low-speeds-part-ii-experim