A Mathematical Model for Helicopter Comprehensive Analysis

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Cite
Pan, Li, and Chen Renliang. “A Mathematical Model for Helicopter Comprehensive Analysis”. Chinese Journal of Aeronautics, vol. 23, no. 3, 2010, pp. 320-6, https://doi.org/10.1016/s1000-9361(09)60222-3.
Pan, L., & Renliang, C. (2010). A Mathematical Model for Helicopter Comprehensive Analysis. Chinese Journal of Aeronautics, 23(3), 320-326. https://doi.org/10.1016/s1000-9361(09)60222-3
Pan L, Renliang C. A Mathematical Model for Helicopter Comprehensive Analysis. Chinese Journal of Aeronautics. 2010;23(3):320-6.
Journal Categories
Technology
Engineering (General)
Civil engineering (General)
Technology
Motor vehicles
Aeronautics
Astronautics
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Refrences
Title Journal Journal Categories Citations Publication Date
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  • Technology: Motor vehicles. Aeronautics. Astronautics
  • Science
  • Technology: Motor vehicles. Aeronautics. Astronautics
  • Technology: Engineering (General). Civil engineering (General)
 88 2006
State-Space Representation of Vortex Wakes by the Method of Lines Journal of the American Helicopter Society 6 2005
Helicopter rotor blade aeroelasticity in forward flight with an implicit structural formulation AIAA Journal
  • Technology: Motor vehicles. Aeronautics. Astronautics
  • Science
  • Technology: Motor vehicles. Aeronautics. Astronautics
  • Technology: Engineering (General). Civil engineering (General)
 12 1992
Effects of hingeless rotor aeroelasticity on helicopter longitudinal flight dynamics 1991
Unsteady rotor airloads prediction using a comprehensive aeroelastic analysis 2003