BALANCING AN AIRCRAFT WITH SYMMETRICALLY DEFLECTED SPLIT ELEVATOR AND RUDDER DURING SHORT LANDING RUN.
- Published in:
- Aviation (1648-7788), 2019, v. 23, n. 1, p. 23, doi. 10.3846/aviation.2019.10301
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- Publication type:
- Article
Works by BA ZUHAIR, Mohammed
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