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Review of Variable Leading Edge Patents for Aircraft Wings and Engine Inlets and Their Relevance for Variable Pitot Inlets in Future Supersonic Transport

  • The motivation for designing variable pitot inlets for future supersonic transport (SST) is explained. A comprehensive overview of existing technological solutions for variable leading edges of aircraft wings and engines inlets is given. The advantages and limitations of over 80 solutions, as well as their relevance for application on variable pitot inlets for SST are analysed. These analyses emphasis challenges of existing solution options concerning design methodologies, level of detail and experience with a technology.

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Metadaten
Author: Stefan KazulaORCiD, Klaus HöschlerGND
URL:https://dlrk2020.dglr.de/programmheft/index.html
Title of the source (German):Deutscher Luft- und Raumfahrtkongress 2020, Online, 1. bis 3. September 2020
Document Type:Conference publication not peer-reviewed
Language:English
Year of publication:2020
Faculty/Chair:Fakultät 3 Maschinenbau, Elektro- und Energiesysteme / FG Flug-Triebwerksdesign
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