Works matching IS 20668201 AND DT 2020 AND VI 12 AND IP 3
Results: 20
Structured Contact Turbulence versus Corona virus Pandemic.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 77, doi. 10.13111/2066-8201.2020.12.3.6
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Design and Development of Multirotor UAV with Automatic Collision Avoidance using Stereo Camera.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 65, doi. 10.13111/2066-8201.2020.12.3.5
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The Influence of Temperature on the Strength of Hybrid Metal-Composite Multi-Bolts Joints.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 49, doi. 10.13111/2066-8201.2020.12.3.4
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Mathematical review of the attitude control mechanism for a spacecraft.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 33, doi. 10.13111/2066-8201.2020.12.3.3
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Mathematical description of the bulk fluid flow and that of the contained impurity dispersion which uses Caputo or Riemann-Liouville fractional order partial derivatives is nonobjective.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 17, doi. 10.13111/2066-8201.2020.12.3.2
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Fabrication and Investigation of Al2024-B4c-Tic Hybrid Metal Matrix Composites using Laser Beam Machining.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 229, doi. 10.13111/2066-8201.2020.12.3.19
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Wear Behaviour of SAE 4340 Steel in Comparison with Single Test Specimen.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 219, doi. 10.13111/2066-8201.2020.12.3.18
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Errors and uncertainties in simulation of steady, viscous flow past a circular cylinder at Re = 20 using a systematic approach.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 203, doi. 10.13111/2066-8201.2020.12.3.17
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Investigation and Joint effect Analysis of Ti-6AL-4V & SS-304L in Aerospace Applications.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 195, doi. 10.13111/2066-8201.2020.12.3.16
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Multi objective optimization of process parameters of AA2014 Friction Stir Weldments using Genetic Algorithm.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 183, doi. 10.13111/2066-8201.2020.12.3.15
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Design of Satellite Attitude Control Systems using Adaptive Neural Networks.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 173, doi. 10.13111/2066-8201.2020.12.3.14
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The effect of the obstacle on the hydraulic response of the composite hydraulic structure.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 151, doi. 10.13111/2066-8201.2020.12.3.13
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Aviation Risk Assessment in the Context of Uncertainty.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 237, doi. 10.13111/2066-8201.2020.12.3.20
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High concentration hydrogen peroxide for rocket fuel applications.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 151, doi. 10.13111/2066-8201.2020.12.3.12
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Weights and sizing assessment in the context of small launcher design.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 137, doi. 10.13111/2066-8201.2020.12.3.11
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A Research on the Performance, Emission and Combustion Parameters of the Hydrogen and Biogas Dual Fuel Engine.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 129, doi. 10.13111/2066-8201.2020.12.3.10
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Analysis of close approach and collision probability between operational satellites and/or space debris.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 113, doi. 10.13111/2066-8201.2020.12.3.9
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Experimental Study on Performance, Emissions and Combustion Characteristics of PFI Spark Ignition Engine Fueled with E30 Equivalent Binary and Ternary GEM Blends.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 101, doi. 10.13111/2066-8201.2020.12.3.8
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Flow Field Study of Bio-Inspired Corrugated Airfoils at Low Reynolds Number with Different Peak Shapes.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 87, doi. 10.13111/2066-8201.2020.12.3.7
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Modelling and Analysis Library Development for Helicopter Blade and Slender Wings.
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- INCAS Bulletin, 2020, v. 12, n. 3, p. 3, doi. 10.13111/2066-8201.2020.12.3.1
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