Dynamical Analysis of Rotor Loads in Helicopter Circling Flight Condition

Author:

Zhou Xu,Zhang Xiayang,Wang Bo,Zhao Qijun

Publisher

Springer Nature Singapore

Reference16 articles.

1. Battey LS (2018) A hybrid navier stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers. Georgia Institute of Technology

2. Deng S, Jiang C, Wang Y et al (2018) Helicopter flight dynamics simulation with continues-time unsteady vortex lattice-free wake and multibody dynamics. In: Asia-Pacific international symposium on aerospace technology

3. Ferhatoglu E, Cigeroglu E, Nevzat zguven H (2018) A new model superposition method for nonlinear vibration analysis of structure using hybrid mode shapes. Mech Syst Sig Process 107(July):317–342

4. Hodges D (1974) Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades. NASA TN D-7818

5. Houbolt B (1958) Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades. NASA Report 1346

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