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METHODOLOGY OF DROP TESTS OF HELICOPTER SKID LANDING GEAR

巻 43, 発行 6, 2012, pp. 835-849
DOI: 10.1615/TsAGISciJ.2013007334
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要約

General data on the testing of skid landing gear for domestic helicopters and the research results on regular patterns of landing impact energy absorption by the skid landing gear are presented. Recommendations for the conditions of the main drop test for this type of landing gear are given.

参考
  1. Aleksandrin, Yu. S. and Timokhin, V. P. , Technique and some results of investigation of the peculiarities of characteristics of helicopter landing impact with the account for properties of landing place surface: Rotorcraft.

  2. Annet, M. S. , LS-DYNA analysis of full-scale helicopters crash test.

  3. Astakhov, M. F., Karavaev, A. V., Makarov, S. Ya., and Suzdaltsev, Ya. Ya. , Guide Book on the Aircraft Calculation for Strength.

  4. Interstate Aviation Committee (IAC), Airworthiness Standards for Normal Category Rotorcraft Aviation Regulations, Part 27.

  5. Interstate Aviation Committee (IAC), Airworthiness Standards: Transport Category Rotorcraft, Aviation Regulations: Part 29.

  6. Korotkov, L. V. , Computational–experimental support for designing and drop tests of helicopter skid landing gear.

  7. Mikhailov, S. A., Korotkov, L. V., Alimov, S. A., and Nedelko, D. V. , Modeling of landing of a helicopter with skid undercarriage with regard for the second landing impact.

  8. Nedelko, D. V. , The energy analysis laboriousness of springs helicopter skid landing gear on results of drop tests.

  9. Pavlov, V. A., Mikhailov, S. A., and Gainutdinov, V. G. , Theory of large and finite pin displacements.

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