Works matching IS 20668201 AND DT 2019 AND VI 11 AND IP 3
Results: 21
Model for self-assessment of an organization's ability to achieve sustained success.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 229, doi. 10.13111/2066-8201.2019.11.3.20
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Numerical simulation of K-, N- and O-regime boundary-layer transition at early nonlinear stage.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 77, doi. 10.13111/2066-8201.2019.11.3.7
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Key Performance Indicators to describe production activity with QTS-2 equipment.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 223, doi. 10.13111/2066-8201.2019.11.3.19
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Assessment of Mechanical Properties of Biocomposite Material by using Sawdust and Rice Husk.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 147, doi. 10.13111/2066-8201.2019.11.3.13
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The hexapod robot for aircraft fuel tank and the use of calculation in the analysis of the effectiveness of radio interference.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 67, doi. 10.13111/2066-8201.2019.11.3.6
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Project management templates used to plan and manage product and service provision. Case study.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 239, doi. 10.13111/2066-8201.2019.11.3.21
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Modeling Fluid dynamics and Aerodynamics by Second Law and Bejan Number (Part 1 - Theory).
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 169, doi. 10.13111/2066-8201.2019.11.3.15
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A short bibliographic report on Small UAV design.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 157, doi. 10.13111/2066-8201.2019.11.3.14
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FAI First Article Inspection in production activity.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 209, doi. 10.13111/2066-8201.2019.11.3.18
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Responsibility of the Russian Federation for Shooting Down a Malaysian Passenger Aircraft on 17<sup>th</sup> July 2014.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 199, doi. 10.13111/2066-8201.2019.11.3.17
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Comparative Review Study of Military and Civilian Unmanned Aerial Vehicles (UAVs).
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 183, doi. 10.13111/2066-8201.2019.11.3.16
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GNSS Navigation Threats Management on-Board of Aircraft.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 111, doi. 10.13111/2066-8201.2019.11.3.10
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The design and performance on 200N-class bipropellant rocket engine using decomposed H<sub>2</sub>O<sub>2</sub> and Kerosene.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 99, doi. 10.13111/2066-8201.2019.11.3.9
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Determination of flow front velocity and optimal injection pressures for better impregnation of E-glass with polyester in resin transfer mold.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 87, doi. 10.13111/2066-8201.2019.11.3.8
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Liquid rocket engine performance assessment in the context of small launcher optimisation.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 135, doi. 10.13111/2066-8201.2019.11.3.12
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Measurement system for the parameters of satellite propulsion.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 127, doi. 10.13111/2066-8201.2019.11.3.11
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An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds Number.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 55, doi. 10.13111/2066-8201.2019.11.3.5
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Existence and static stability of a capillary free surface appearing in a dewetted Bridgman process. Part I.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 29, doi. 10.13111/2066-8201.2019.11.3.3
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Numerical Methods for Transverse Vibration Analysis of Straight Euler and Timoshenko Beams.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 15, doi. 10.13111/2066-8201.2019.11.3.2
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Tuning of the Wavelet Filters for the IMU Data Based on the PDC Method and the GPS Solution in a Bi-Dimensional Navigation Application.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 3, doi. 10.13111/2066-8201.2019.11.3.1
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Unmanned aero-amphibious vehicle: preliminary study on conceptual design.
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- INCAS Bulletin, 2019, v. 11, n. 3, p. 41, doi. 10.13111/2066-8201.2019.11.3.4
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- Article