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Algorithms for controlling fatigue tests of airplanes. (English. Russian original) Zbl 1284.74036

J. Appl. Mech. Tech. Phys. 55, No. 1, 164-171 (2014); translation from Prikl. Mekh. Tekh. Fiz. 55, No. 1, 198-206 (2014).
Summary: The efficiency of algorithms for automatic control of forces prescribed in the test program is analyzed by an example of a large-aspect-ratio wing considered as a beam loaded by aerodynamic and inertial forces.

MSC:

74F10 Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.)
74K10 Rods (beams, columns, shafts, arches, rings, etc.)
76G25 General aerodynamics and subsonic flows
93C85 Automated systems (robots, etc.) in control theory
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References:

[1] V. L. Prisekin and G. I. Rastorguev, ”Algorithm of Controlling the Strength Tests of the Airplane Structure,” Nauch. Vestn. Novosib. Gos. Tekh. Univ., No. 1, 75–82 (2012).
[2] V. L. Prisekin, N. V. Pustovoi, A. I. Belousov, and Yu. B. Nigirich, ”Computer Model of a Test Rig and Airplane for Strength Tests,” Nauch. Vestn. Novosib. Gos. Tekh. Univ., No. 1, 3–11 (1996).
[3] V. L. Prisekin, G. I. Rastorguev, and A. I. Belousov, ”Calculation of the Compliance Matrix of the Structure Based on Experimental Data,” in Selected Problems of Strength of Modern Engineering, Collected Papers Devoted to the 85th Anniversary of E. I. Grigolyuk (1923–2005) (Inst. Mechanics at the Moscow State University, Fizmatlit, Moscow, 2008), pp. 56–60.
[4] V. L. Prisekin and A. I. Belousov, ”Algorithms of Loading Control in Test Rigs,” Nauch. Vestn. Novosib. Gos. Tekh. Univ., No. 1, 3–11 (2000).
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