Works matching IS 20668201 AND DT 2017 AND VI 9 AND IP 4
Results: 10
Cessna Citation X Business Aircraft Eigenvalue Stability - Part 1: a New GUI for the LFRs Generation.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 31, doi. 10.13111/2066-8201.2017.9.4.4
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- Article
Supersonic and transonic Mach probe for calibration control in the Trisonic Wind Tunnel.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 113, doi. 10.13111/2066-8201.2017.9.4.10
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- Article
Stability analysis for an UAV model in a longitudinal flight.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 21, doi. 10.13111/2066-8201.2017.9.4.3
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- Article
The Origin of Shear Turbulence.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 75, doi. 10.13111/2066-8201.2017.9.4.7
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- Article
Comparative Analysis Program for Experimental and Calculated Data.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 59, doi. 10.13111/2066-8201.2017.9.4.6
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- Article
Drop dispensing in a viscous outer liquid.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 101, doi. 10.13111/2066-8201.2017.9.4.9
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- Article
Cessna Citation X Business Aircraft Eigenvalue Stability - Part2: Flight Envelope Analysis.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 45, doi. 10.13111/2066-8201.2017.9.4.5
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- Article
Controlling the Motion of a Planar 3-DOF Manipulator Using PID Controllers.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 91, doi. 10.13111/2066-8201.2017.9.4.8
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- Article
Possible Simple Structures of the Universe to Include General Relativity Effects.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 11, doi. 10.13111/2066-8201.2017.9.4.2
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- Article
Integral Method for Static, Dynamic, Stability and Aeroelastic Analysis of Beam-like Structure Configurations.
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- INCAS Bulletin, 2017, v. 9, n. 4, p. 3, doi. 10.13111/2066-8201.2017.9.4.1
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- Article