Antonio Ferri (German Wikipedia)

Analysis of information sources in references of the Wikipedia article "Antonio Ferri" in German language version.

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  • Patent US2990142AA: Scoop-Type Supersonic Inlet With Precompression Surface. Angemeldet am 11. Mai 1955, veröffentlicht am 27. Juni 1961, Anmelder: Curtiss Wright Corp, Erfinder: Antonio Ferri. „An object of this invention is to provide a novel construction of a scoop-type supersonic air inlet for the efficient conversion of dynamic pressure to static pressure. A further object of this invention is to provide a novel construction to facilitate starting of a scoop-type supersonic air inlet. Increases in static pressure, or compression, in a supersonic inlet can be accomplished by the physical turning of the air which results in the generation of compressive shock waves. A further object of the invention comprises the provision of a scoop-type air inlet having a novel aerodynamic compression surface (hereinafter termed a compression bump) for more efficiently producing compression in the inlet.“

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  • United States National Advisory Committee for Aeronautics (Hrsg.): Report – National Advisory Committee for Aeronautics, Ausgaben 863–891. U.S. Government Printing Office, 1947, S. 61 (eingeschränkte Vorschau in der Google-Buchsuche).
  • Favorable Interference. In: United States Air Force Director of Research Programs (Hrsg.): United States Air Force Research Accomplishments. Band 64, Nr. 6. USAF Office of Aerospace Research, 1964, S. II-G-11 (eingeschränkte Vorschau in der Google-Buchsuche): „The authors would like to acknowledge the help of Dr. Antonio Ferri who, it is believed, first suggested the concept of a contoured surface or ‚bump‘ ahead of an inlet. The many published works of A. Ferri proved invaluable in the formulation of the theoretical methods. […] The concept of a contoured or ‚bump‘ surface as a combination precompression surface and boundary-layer removal device is presented as an aid to high-speed inlet design.“
  • Antonio Ferri: A Review of Some Recent Developments in Hypersonic Flow. In: United States Air Force (Hrsg.): WADC Technical Note. Band 58, Nr. 230. Wright Air Development Center, Air Research and Development Command, 1958 (eingeschränkte Vorschau in der Google-Buchsuche).
  • Paul A. Libby: Observations Concerning Supersonic Combustion. In: M. Champion, B. Deshaies (Hrsg.): IUTAM Symposium on Combustion in Supersonic Flows – Proceedings of the IUTAM Symposium held in Poitiers, France, 2–6 October 1995 (= Band 39 von Fluid Mechanics and Its Applications). Springer Science & Business Media, 1995, ISBN 978-94-011-5432-1, S. 1–3 (eingeschränkte Vorschau in der Google-Buchsuche).

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