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Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations
Research article (Aerospace Science and Technology, 2019) · cited 12× · AI/ML
Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations
Summary
Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations is a scholarly article[1].
Key Facts
Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations's instance of is recorded as scholarly article[2].
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APA4ort.xyz Knowledge Graph. (2026). Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations. Retrieved May 24, 2026, from https://4ort.xyz/entity/control-device-effectiveness-studies-of-a-53-swept-flying-wing-configuration-experimental-computational-and-modeling-con
MLA“Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/control-device-effectiveness-studies-of-a-53-swept-flying-wing-configuration-experimental-computational-and-modeling-con.
BibTeX@misc{4ortxyz_control-device-effectiveness-studies-of-a-53-swept-flying-wing-configuration-experimental-computational-and-modeling-con_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations}}, year = {2026}, url = {https://4ort.xyz/entity/control-device-effectiveness-studies-of-a-53-swept-flying-wing-configuration-experimental-computational-and-modeling-con}, note = {Accessed: 2026-05-24}}
LLM promptAccording to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations — https://4ort.xyz/entity/control-device-effectiveness-studies-of-a-53-swept-flying-wing-configuration-experimental-computational-and-modeling-con (retrieved 2026-05-24)