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00:46 Mar 23, 2018 |
Polish to English translations [PRO] Tech/Engineering - Aerospace / Aviation / Space / airplanes | |||||||
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| Selected response from: Frank Szmulowicz, Ph. D. United States Local time: 00:08 | ||||||
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Summary of answers provided | ||||
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3 | stabilizer attachment point |
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Discussion entries: 3 | |
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stabilizer attachment point Explanation: Stykówka, IMO, jest miejscem styku dwóch części, na przykład, odnośnie samolotu MIG: "stykówce" czyli w miejscu łączenia tylnej i przedniej części kadłuba. http://pwm.org.pl/viewtopic.php?f=13&t=3722 ccccccccccccccccccccccc Two gray scale amplitude C-scan images of the section of the horizontal stabilizer are presented in figures 5 and 6: a section encompassing the outer edge corner of the stabilizer (576 mm x 298 mm), and a section near the attachment point of the stabilizer to the airplane fuselage (450 mm x 360 mm). https://www.google.com/search?num=100&ei=r1e0WtnkBY29jwS0mJT... c An aircraft stabilizer is an aerodynamic surface, typically including one or more movable control surfaces,[1][2] that provides longitudinal (pitch) and/or directional (yaw) stability and control. A stabilizer can feature a fixed or adjustable structure on which any movable control surfaces are hinged, or it can itself be a fully movable surface such as a stabilator. Depending on the context, "stabilizer" may sometimes describe only the front part of the overall surface https://upload.wikimedia.org/wikipedia/commons/thumb/7/76/Ta... |
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