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ROPE SYSTEM PARAMETRIC CONFIGURATION FOR AIRCRAFT TOWING WITH GUARANTEED VERTICAL SHIFT RANGE

卷 40, 册 3, 2009, pp. 379-391
DOI: 10.1615/TsAGISciJ.v40.i3.80
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摘要

Steady motion of a low-sized vehicle connected via flexible rope to a horizontally flying airplane-carrier is considered. Rope system parameters are determined to provide the maximum range of vertical shifts of the apparatus relative to the carrier in the entire region of the carrier's horizontal flight regimes.

参考文献
  1. Gorshkov, A. S., Krivol's Formula Generalization to Calculate Flexible Rope Tension and Form in a Flow.

  2. Schlichting, H., Boundary-Layer Theory.

  3. Lebedev, A. A., Flight Dynamics.

  4. Morozov, L. V., The conditions of numerical solution guaranteed convergence for the boundary problem of the equilibrium state of the air-tug flexible rope.

  5. Vasiliev, Ph. P., Numerical Methods for Extremum Problems.

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