BALANCING AN AIRCRAFT WITH SYMMETRICALLY DEFLECTED SPLIT ELEVATOR AND RUDDER DURING SHORT LANDING RUN.
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- Aviation (1648-7788), 2019, v. 23, n. 1, p. 23, doi. 10.3846/aviation.2019.10301
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- Article
Works matching IS 1648-7788 AND VI 23 AND IP 1 AND DT 2019
Results: 5
1
2
ROBUST CONTROLLER FOR SUPERSONIC UNMANNED AERIAL VEHICLE.
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- Aviation (1648-7788), 2019, v. 23, n. 1, p. 31, doi. 10.3846/aviation.2019.10300
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- Publication type:
- Article
3
NUMBER OF CONFLICTS AT THE ROUTE INTERSECTION -- MINIMUM DISTANCE MODEL.
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- Aviation (1648-7788), 2019, v. 23, n. 1, p. 1, doi. 10.3846/aviation.2019.9746
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- Publication type:
- Article
4
PROCESS MODELING OF CARBON-EPOXY COMPOSITES: RESIDUAL STRESS DEVELOPMENT DURING CURE AND ANALYSIS OF FREE EDGE EFFECTS.
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- Aviation (1648-7788), 2019, v. 23, n. 1, p. 15, doi. 10.3846/aviation.2019.9745
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- Publication type:
- Article
5
SAFETY AND THE ECONOMIC AND FINANCIAL PERFORMANCE IN THE AIRLINE INDUSTRY: IS THERE ANY RELATIONSHIP?
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- Aviation (1648-7788), 2019, v. 23, n. 1, p. 7, doi. 10.3846/aviation.2019.9744
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- Article