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Cited by
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This article has been cited by the following publications. This list is generated based on data provided by Crossref.
Ali, F. Tzanidakis, K. Goulos, I. Pachidis, V. and d’Ippolito, R. 2015. Multidisciplinary design and optimisation of conceptual rotorcraft powerplants for operational performance and environmental impact. The Aeronautical Journal, Vol. 119, Issue. 1217, p. 891.
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Goulos, I. 2015. Modelling the aeroelastic response and flight dynamics of a hingeless rotor helicopter including the effects of rotor-fuselage aerodynamic interaction. The Aeronautical Journal, Vol. 119, Issue. 1214, p. 433.
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Castillo Pardo, Alejandro Goulos, Ioannis and Pachidis, Vassilios 2017. Modelling and analysis of coupled flap-lag-torsion vibration characteristics helicopter rotor blades. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 231, Issue. 10, p. 1804.
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Goulos, Ioannis and Bonesso, Marco 2019. Variable rotor speed and active blade twist for civil rotorcraft: Optimum scheduling, mission analysis, and environmental impact. Aerospace Science and Technology, Vol. 88, Issue. , p. 444.
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Sarker, Pratik and Chakravarty, Uttam K. 2021. On the dynamic response of a hingeless helicopter rotor blade. Aerospace Science and Technology, Vol. 115, Issue. , p. 106741.
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Flexible rotor blade dynamics for helicopter aeromechanics including comparisons with experimental data
  • Volume 119, Issue 1213
  • I. Goulos, V. Pachidis (a1) and P. Pilidis (a1)
  • DOI: https://doi.org/10.1017/S0001924000010496
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Flexible rotor blade dynamics for helicopter aeromechanics including comparisons with experimental data
  • Volume 119, Issue 1213
  • I. Goulos, V. Pachidis (a1) and P. Pilidis (a1)
  • DOI: https://doi.org/10.1017/S0001924000010496
Available formats Please select a format to save.
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Flexible rotor blade dynamics for helicopter aeromechanics including comparisons with experimental data
  • Volume 119, Issue 1213
  • I. Goulos, V. Pachidis (a1) and P. Pilidis (a1)
  • DOI: https://doi.org/10.1017/S0001924000010496
Available formats Please select a format to save.
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