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- W2321811884 abstract "This paper discusses the basic design approach and features of the turbotip lift fan concept, initially developed for application in the XV-5 VTOL research aircraft. Design changes necessary to meet the requirements of the proposed NASA V/STOL transport research aircraft and future commercial transport systems are reviewed. Emphasis is placed on the effects of acoustic, installation, control response and life/maintenance objectives on component design and lift fan geometry." @default.
- W2321811884 created "2016-06-24" @default.
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- W2321811884 date "1972-03-26" @default.
- W2321811884 modified "2023-09-26" @default.
- W2321811884 title "Turbotip Lift Fan Design" @default.
- W2321811884 doi "https://doi.org/10.1115/72-gt-111" @default.
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