Works matching IS 20668201 AND DT 2015 AND VI 7 AND IP 3
Results: 18
The Effects of Fibre Volume Fraction on a Glass-Epoxy Composite Material.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 113, doi. 10.13111/2066-8201.2015.7.3.10
- By:
- Publication type:
- Article
On the evaluation of mechanical properties of honeycombs by using finite element analyses.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 135, doi. 10.13111/2066-8201.2015.7.3.13
- By:
- Publication type:
- Article
A computational study of heat transfer in a laminar oscillating confined slot jet impinging on an isothermal surface at low Reynolds numbers.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 101, doi. 10.13111/2066-8201.2015.7.3.9
- By:
- Publication type:
- Article
Research of Zlin Z42 engine's operation by EDM-800 monitoring system.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 181, doi. 10.13111/2066-8201.2015.7.3.17
- By:
- Publication type:
- Article
An Expedite Approximate Algorithm for Calculating the Controls in the Longitudinal Maneuver.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 121, doi. 10.13111/2066-8201.2015.7.3.11
- By:
- Publication type:
- Article
Overload prevention in model supports for wind tunnel model testing.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 173, doi. 10.13111/2066-8201.2015.7.3.16
- By:
- Publication type:
- Article
Optimizing Armed Forces Capabilities for Hybrid Warfare - New Challenge for Slovak Armed Forces.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 191, doi. 10.13111/2066-8201.2015.7.3.18
- By:
- Publication type:
- Article
Computations of the Shock Waves at Hypersonic Velocities Taken into Account the Chemical Reactions that Appear in the Air at High Temperatures.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 129, doi. 10.13111/2066-8201.2015.7.3.12
- By:
- Publication type:
- Article
Boundary Vorticity Dynamics at Very Large Reynolds Numbers.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 89, doi. 10.13111/2066-8201.2015.7.3.8
- By:
- Publication type:
- Article
Small Orbital Launcher - Risk Zone Evaluation.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 73, doi. 10.13111/2066-8201.2015.7.3.7
- By:
- Publication type:
- Article
Hover flight control of helicopter using optimal control theory.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 11, doi. 10.13111/2066-8201.2015.7.3.2
- By:
- Publication type:
- Article
Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage Part 5: A Panel Method for Non-Lifting Bodies.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 59, doi. 10.13111/2066-8201.2015.7.3.6
- By:
- Publication type:
- Article
Avionics and ATC Technology for Mission Control.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 161, doi. 10.13111/2066-8201.2015.7.3.15
- By:
- Publication type:
- Article
The Sound Attenuation Coefficient Optimization in Case of a Three Parameter Impedance Model for a Rectangular 3D Straight Lined Duct of Finite Dimensions.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 39, doi. 10.13111/2066-8201.2015.7.3.4
- By:
- Publication type:
- Article
Airline Applications of Business Intelligence Systems.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 153, doi. 10.13111/2066-8201.2015.7.3.14
- By:
- Publication type:
- Article
Impact Simulation With an Aircraft Wing Using SPH Bird Model.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 51, doi. 10.13111/2066-8201.2015.7.3.5
- By:
- Publication type:
- Article
Regression Models for Predicting Force Coefficients of Aerofoils.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 3, doi. 10.13111/2066-8201.2015.7.3.1
- By:
- Publication type:
- Article
The completion of the mathematical model by parameter identification for simulating a turbofan engine.
- Published in:
- INCAS Bulletin, 2015, v. 7, n. 3, p. 25, doi. 10.13111/2066-8201.2015.7.3.3
- By:
- Publication type:
- Article