Works matching IS 20668201 AND DT 2019 AND VI 11 AND IP 1
Results: 18
The configuration management requirements for aviation, space and defense organizations.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 239, doi. 10.13111/2066-8201.2019.11.1.19
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Overview regarding the certification of a new military jet aircraft for school and training.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 231, doi. 10.13111/2066-8201.2019.11.1.18
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Air Power as a Security Factor: Case study Syria.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 217, doi. 10.13111/2066-8201.2019.11.1.17
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Considerations on control processes in aeronautical organizations in the context of improving safety and efficiency.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 207, doi. 10.13111/2066-8201.2019.11.1.16
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Nonlinear Lifting-Line Model using a Vector Formulation of the Unsteady Kutta-Joukowski Theorem.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 189, doi. 10.13111/2066-8201.2019.11.1.15
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Validation of a helicopter turbulence model on PUMA 330 dynamics.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 179, doi. 10.13111/2066-8201.2019.11.1.14
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Lightweight vitreous carbon material: approaches to making open-pore cellular structure.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 171, doi. 10.13111/2066-8201.2019.11.1.13
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Missile Grid Fins Analysis using Computational Fluid Dynamics: A Systematic Review.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 151, doi. 10.13111/2066-8201.2019.11.1.12
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Fabrication and testing of various sandwich composites.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 131, doi. 10.13111/2066-8201.2019.11.1.10
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Analytical solutions of a particular Hill's differential system.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 121, doi. 10.13111/2066-8201.2019.11.1.9
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Aerodynamic Performance of Micro Aerial Wing Structures at Low Reynolds Number.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 107, doi. 10.13111/2066-8201.2019.11.1.8
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Using genetic algorithms to optimize airfoils in incompressible regime.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 79, doi. 10.13111/2066-8201.2019.11.1.6
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Estimation of Wind Tunnel Corrections Using Potential Models.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 53, doi. 10.13111/2066-8201.2019.11.1.4
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Prediction of Broadband Noise from Symmetric and Cambered Airfoils.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 39, doi. 10.13111/2066-8201.2019.11.1.3
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Simulation Study of the Aerodynamic Force Distributions on the UAS-S45 Baalam Wing with an Upswept Blended Winglet.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 21, doi. 10.13111/2066-8201.2019.11.1.2
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The structural optimum design of laminated slender beam section with arbitrary material distribution using a genetic algorithm.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 7, doi. 10.13111/2066-8201.2019.11.1.1
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Temperature Effects on Damage Mechanisms of Hybrid Metal - Composite Bolted Joints Using SHM Testing Method.
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- INCAS Bulletin, 2019, v. 11, n. 1, p. 61, doi. 10.13111/2066-8201.2019.11.1.5
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FOREWORD.
- Published in:
- INCAS Bulletin, 2019, v. 11, n. 1, p. 1
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- Article