DETERMINATION OF LOADS IN THE ULTRALIGHT HELICOPTER BLADES.
- Published in:
- Aviation (1648-7788), 2023, v. 27, n. 4, p. 242, doi. 10.3846/aviation.2023.20236
- By:
- Publication type:
- Article
Works matching IS 16487788 AND DT 2023 AND VI 27 AND IP 4
Results: 6
1
2
EFFICIENCY OF POLYMER MATERIALS IN HIGHLY LOADED SYSTEMS IN THE AVIATION INDUSTRY.
- Published in:
- Aviation (1648-7788), 2023, v. 27, n. 4, p. 272, doi. 10.3846/aviation.2023.20650
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- Publication type:
- Article
3
INTEGRATED REPORTING AS A MODEL FOR SUSTAINABILITY MANAGEMENT REPORTING: THE CASE OF NORTHEASTERN EUROPEAN AIRPORTS.
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- Aviation (1648-7788), 2023, v. 27, n. 4, p. 259, doi. 10.3846/aviation.2023.20607
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- Publication type:
- Article
4
DEVELOPING A COMPUTER VISION BASED SYSTEM FOR AUTONOMOUS TAXIING OF AIRCRAFT.
- Published in:
- Aviation (1648-7788), 2023, v. 27, n. 4, p. 248, doi. 10.3846/aviation.2023.20588
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- Publication type:
- Article
5
RATIONAL CONTROL BY TEMPERATURE IN VORTEX ENERGY SEPARATOR UNDER DESTABILIZING EFFECTS.
- Published in:
- Aviation (1648-7788), 2023, v. 27, n. 4, p. 234, doi. 10.3846/aviation.2023.20229
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- Publication type:
- Article
6
CUSTOMER-FOCUSED AIRCRAFT SEAT DESIGN: A CASE STUDY WITH AHP-QFD.
- Published in:
- Aviation (1648-7788), 2023, v. 27, n. 4, p. 225, doi. 10.3846/aviation.2023.20210
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- Publication type:
- Article