Abstract
The paper is concerned with mechanical phenomena accompanying ground run of aircraft with near-critical slip angles. Such phenomena (reduced effectiveness of directional control, self-excited frictional vibrations of a landing gear, internal resonance of an aileron, transverse oscillations of the legs of a multileg landing gear) are due to the nonlinear dependence of the side force on the slip angles
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References
L. L. Antseliovich, Aircraft Reliability, Safety, and Survivability [in Russian], Mashinostroenie, Moscow (1985).
V. L. Biderman, Theory of Mechanical Vibrations [in Russian], Vysshaya Shkola, Moscow (1980).
T. I. Ligum, S. Yu. Skripnichenko, and A. V. Shishmarev, Aerodynamics of the Tu-154B Aircraft [in Russian], Transport, Moscow (1985).
L. G. Lobas and V. G. Verbitskii, Qualitative and Analytic Methods in Dynamics of Wheeled Vehicles [in Russian], Naukova Dumka, Kiev (1990).
V. G. Mikeladze and V. M. Titov, Basic Geometrical and Aerodynamic Characteristics of Aircraft and Rockets [in Russian], Mashinostroenie, Moscow (1990).
N. P. Plakhtienko and B. M. Shifrin, “On the motion stability of an airplane on a runway under wind loading,” Int. Appl. Mech., 35, No. 10, 1068–1075 (1999).
N. P. Plakhtienko and B. M. Shifrin, “On transverse vibration of aircraft landing gear,” Strength of Materials, 34, No. 6, 79–89 (2002).
N. P. Plakhtienko and B. M. Shifrin, “On the nature of one type of self-excited transverse oscillations of aircraft landing gear,” in: Problems of Aircraft Design and Manufacture [in Russian], Issue 27 (4), NAKU, Kharkov (2001), pp. 46–55.
V. A. Trofimov, “Design basis for dampers of transverse vibrations of legs in multileg landing gear,” in: Open Information and Integrated Computer Technologies [in Russian], Issue 13, NAKU, Kharkov (2002), pp. 44–50.
M. J. Abzug, “Directional stability and control during landing rollout,” J. Aircraft, 36, No. 3, 584–590 (1999).
G. Gim and P. E. Nikravesh, “An analytic model of pneumatic tyres for vehicle dynamic simulations. Part 1: Pure slips,” Int. J. Vehicle Design, 11, No. 6, 583–618 (1990).
V. B. Larin, “Motion planning for a wheeled robot (kinematic approximation),” Int. Appl. Mech., 41, No. 2, 187–196 (2005).
V. B. Larin, “Control of wheeled robots,” Int. Appl. Mech., 41, No. 4, 441–448 (2005).
V. B. Larin, “Motion planning for a mobile robot with two steerable wheels,” Int. Appl. Mech., 41, No. 5, 552–559 (2005).
H. Sakai, “Theoretical and experimental studies on the dynamic properties of tires. Part 4: Investigations of the influences of running conditions by calculation and experiment,” Int. J. Vehicle Design, 3, No. 3, 333–375 (1982).
U.K. Patent Application GB, Combined Hinge and Deflection Arrangement for an Aerodynamics Control Member, Int. CI.B64C9/02 F16C 11/06, British Aerospace Pic., London (1983).
V. G. Verbitskii, V. A. Makarov, and V. P. Sakhno, “Influence of the asymmetry of cornering forces on the static stability of a two-axle vehicle,” Int. Appl. Mech., 40, No. 11, 1304–1309 (2004).
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Translated from Prikladnaya Mekhanika, Vol. 42, No. 6, pp. 128–135, June 2006.
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Plakhtienko, N.P., Shifrin, B.M. Mechanical phenomena in ground run of an aircraft with near-critical slip angles. Int Appl Mech 42, 714–720 (2006). https://doi.org/10.1007/s10778-006-0139-3
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DOI: https://doi.org/10.1007/s10778-006-0139-3