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METHODS OF SOLVING THE EQUATION OF HELICOPTER ROTOR ELASTIC BLADE MOTION IN THE GENERAL CASE

Volume 41, Issue 5, 2010, pp. 593-610
DOI: 10.1615/TsAGISciJ.v41.i5.80
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ABSTRACT

Given in this paper is the method of computation of helicopter rotor elastic blade motion in the general case. Comparisons of the results of computations based on the present method to the results of wind tunnel and flight tests are presented. The method can be used in the determination of aerodynamic and aeroelastic characteristics of main and tail rotors for a wide range of problems concerning helicopter aeromechanics.

REFERENCES
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  2. Baskin, V. E., Vildgrube, L. S., Vozhdayev, E. S., and Maykopar, G. I., Burtsev, B. N., Method of Calculating of the Loads on the Blades and in the Control System of Coaxial Rotor Helicopter.

  3. Johnson, W., Helicopter Theory.

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CITED BY
  1. Rybkin P. N., Сhinynchin Yu. M., To the problem of simulation modelling of abnormal and emergency flight situations in the process of Mi-8MTV helicopter pilot simulation training, Civil Aviation High Technologies, 25, 5, 2022. Crossref

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