Fuselage-Induced Velocity Model for LRTA, RTA, and HART Fuselages

A model for real-time computation of fuselage-rotor interference

BG van der Wall, J Yin - International Journal of Modeling …, 2017 - World Scientific
A simple analytical real-time capable model to account for fuselage-induced velocities at
rotor blade elements is described at the example of the Bo105 fuselage. Data of the …
被引用次数：1 相关文章 所有 3 个版本
[PDF] nasa.gov

A simple analytical fuselage-induced velocity model for comprehensive rotor codes

BG van der Wall, M Wentrup, G Rajagopalan… - European Rotorcraft …, 2015 - ntrs.nasa.gov
A simple analytical model to account for fuselage-induced velocities at rotor blade elements
and at rotor wake nodes is described. The method is applied to three different fuselage …
被引用次数：1 相关文章 所有 7 个版本