AERO DAY 2025, The virtual twin experience for aerospace CENIT - DASSAULT SYSTÈMES - INCAS.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 145, doi. 10.13111/2066-8201.2025.17.2.13
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Works in INCAS Bulletin, 2025, Vol 17, Issue 2
Results: 13
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A CS-23 Compliant Light Aircraft with Integrated Garmin Avionics: Safety, Simplicity, and Sustainability.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 135, doi. 10.13111/2066-8201.2025.17.2.12
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- Article
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Key Considerations in the Design of a New EASA CS-23 General Aviation Aircraft.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 119, doi. 10.13111/2066-8201.2025.17.2.11
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- Article
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The Relative Inertiality - The Relative Mechanical Movement of Bodies in Outer Space.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 105, doi. 10.13111/2066-8201.2025.17.2.10
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- Article
5
The pulsatory liposome works as a neuronal network (II).
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 97, doi. 10.13111/2066-8201.2025.17.2.9
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- Article
6
Lunar Rickshaw - A non-Motorized Vehicle Designed for Exploration and Rescue Missions on the Moon's South Pole.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 77, doi. 10.13111/2066-8201.2025.17.2.8
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- Article
7
Influence of the mechanical properties of nanoparticles on epoxy resin L.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 67, doi. 10.13111/2066-8201.2025.17.2.7
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- Article
8
Brief foray into practical high sensitivity magnetometry, a method for weak magnetic field survey, magnetic storms monitoring and possible extensions to airspace defense.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 59, doi. 10.13111/2066-8201.2025.17.2.6
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9
Comparison of Aerodynamic Characteristics of Morphing and Conventional Wings.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 47, doi. 10.13111/2066-8201.2025.17.2.5
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- Article
10
Design Exploration of the NACA Airfoil Family Using High-Fidelity CFD Analysis.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 35, doi. 10.13111/2066-8201.2025.17.2.4
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11
Stability of flexible orbital structures.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 23, doi. 10.13111/2066-8201.2025.17.2.3
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12
Mathematical Modelling and Structural Stability in Aerospace.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 13, doi. 10.13111/2066-8201.2025.17.2.2
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13
Effect of Coremat Xi 3 Middle Layer on Flexural Performance of Glass Fibre Composites under Different Test Rates.
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- INCAS Bulletin, 2025, v. 17, n. 2, p. 3, doi. 10.13111/2066-8201.2025.17.2.1
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- Article