A STUDY OF HIGH LIFT AERODYNAMIC DEVICES ON COMMERCIAL AIRCRAFTS.
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- Aviation (1648-7788), 2020, v. 24, n. 3, p. 123, doi. 10.3846/aviation.2020.12815
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Works matching IS 16487788 AND DT 2020 AND VI 24 AND IP 3
Results: 5
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2
ASPECTS OF COMPLEXITY OF METAL-FIBROUS MICROSTRUCTURE FOR THE CONSTRUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS: ESTIMATION OF ADHESIVE STRENGTH.
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- Aviation (1648-7788), 2020, v. 24, n. 3, p. 117, doi. 10.3846/aviation.2020.11978
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- Article
3
GRADIENT-BASED OPTIMIZATION OF SPACECRAFT AND AIRCRAFT THERMAL DESIGN.
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- Aviation (1648-7788), 2020, v. 24, n. 3, p. 105, doi. 10.3846/aviation.2020.13045
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- Publication type:
- Article
4
ASPECTS OF COMPLEXITY OF METAL-FIBROUS MICROSTRUCTURE FOR THE CONSTRUCTION OF HIGH-PERFORMANCE HEAT EXCHANGERS: THERMAL PROPERTIES.
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- Aviation (1648-7788), 2020, v. 24, n. 3, p. 99, doi. 10.3846/aviation.2020.12086
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- Publication type:
- Article
5
AIRPORT TYPOLOGY FOR LCC POLICY CHANGES: A EUROPEAN PERSPECTIVE.
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- Aviation (1648-7788), 2020, v. 24, n. 3, p. 90, doi. 10.3846/aviation.2020.12051
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- Article