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- W2319291569 abstract "The X-22A aircraft was evaluated to establish the status of its development and its potential usefulness for conducting flight research using a variable stability system. The more significant aspects and results of the tests are covered in this paper. Ground familiarization and planning conducted prior to the flight tests included the use of a fixed-based simulator programmed with X-22A design data. Test techniques were developed and/or refined during both ground simulator work and actual flight tests as necessary to adapt to the unique characteristics of the aircraft. Quantitative and qualitative evaluation of the stability and control characteristics in terms of their effect on the aircraft to perform its intended mission of flight research have shown that it is acceptable in all respects considered. Unusually high sideforce, with no means of variation, was the most detrimental characteristic of the aircraft noted relative to its potential use as a variable stability flight research vehicle." @default.
- W2319291569 created "2016-06-24" @default.
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- W2319291569 date "1969-03-10" @default.
- W2319291569 modified "2023-09-26" @default.
- W2319291569 title "Initial military flight tests of the X-22A VSTOL research aircraft" @default.
- W2319291569 doi "https://doi.org/10.2514/6.1969-319" @default.
- W2319291569 hasPublicationYear "1969" @default.
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