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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
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
Summary
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 is a scholarly article[1].
Key Facts
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's instance of is recorded as scholarly article[2].
References
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Use these citations when quoting this entity in research, articles, AI prompts, or wherever provenance matters. We aggregate Wikidata + Wikipedia + authoritative open-data sources; the stitched, scored, cross-referenced view is what 4ort.xyz contributes.
APA4ort.xyz Knowledge Graph. (2026). 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. Retrieved May 24, 2026, from https://4ort.xyz/entity/optimization-and-design-of-an-aircraft-s-morphing-wing-tip-demonstrator-for-drag-reduction-at-low-speeds-part-ii-experim
MLA“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.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/optimization-and-design-of-an-aircraft-s-morphing-wing-tip-demonstrator-for-drag-reduction-at-low-speeds-part-ii-experim.
BibTeX@misc{4ortxyz_optimization-and-design-of-an-aircraft-s-morphing-wing-tip-demonstrator-for-drag-reduction-at-low-speeds-part-ii-experim_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{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}}, year = {2026}, url = {https://4ort.xyz/entity/optimization-and-design-of-an-aircraft-s-morphing-wing-tip-demonstrator-for-drag-reduction-at-low-speeds-part-ii-experim}, note = {Accessed: 2026-05-24}}
LLM promptAccording to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): 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 — https://4ort.xyz/entity/optimization-and-design-of-an-aircraft-s-morphing-wing-tip-demonstrator-for-drag-reduction-at-low-speeds-part-ii-experim (retrieved 2026-05-24)
