20th 2001 ASME Wind Energy Symposium 2001
DOI: 10.2514/6.2001-61
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Exploratory study of HAWT blade throw risk to nearby people and property

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Cited by 8 publications
(8 citation statements)
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“…Turner, 3 also employing a point-mass model, used Monte Carlo simulation techniques to construct a statistical distribution of blade fragment impact. Eggers et al 4 likewise exercised a point-mass model for blade fragments using Monte Carlo methods and obtained results similar to that of Macqueen et al 2 The first investigation of fragment throw using full six-degree-of-freedom modeling was performed by Montgomerie, 5 who reported very high maximum distances. Sørensen 6,7 also analysed full rigid body motion of the blade fragment and reported how maximum throw distance varied as a function of aerodynamic characteristics, fragment center of gravity location, pitch angle and wind velocity.…”
Section: Introductionmentioning
confidence: 76%
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“…Turner, 3 also employing a point-mass model, used Monte Carlo simulation techniques to construct a statistical distribution of blade fragment impact. Eggers et al 4 likewise exercised a point-mass model for blade fragments using Monte Carlo methods and obtained results similar to that of Macqueen et al 2 The first investigation of fragment throw using full six-degree-of-freedom modeling was performed by Montgomerie, 5 who reported very high maximum distances. Sørensen 6,7 also analysed full rigid body motion of the blade fragment and reported how maximum throw distance varied as a function of aerodynamic characteristics, fragment center of gravity location, pitch angle and wind velocity.…”
Section: Introductionmentioning
confidence: 76%
“…The dynamic model of the blade fragment in free flight consists of 13 scalar differential equations, given by equations (1)- (4). The states of the system are defined as follows: blade mass center position with respect to the inertial frame (x; y; z), mass center translational velocity resolved in the blade-fixed frame (u; v; w), quaternion rotational parameters describing blade orientation (q 0 ; q 1 ; q 2 ; q 3 ) and angular velocity components resolved in the blade-fixed frame (p; q; r).…”
Section: Blade Throw Dynamic Modelmentioning
confidence: 99%
“…Notice that X, Y, Z are the body frame components of the total applied forces while L, M, N represent the body frame applied moments about the mass center. The mass of the rotor blade is denoted as m. The matrix [T IB ] is the body to inertial frame rotation transformation matrix given by (5) and [I ] is the mass moment of inertia matrix of the body evaluated at the mass center with respect to body frame coordinates.…”
Section: Dynamic Model Of a Rotor Blade Failure 21 Blade Equations mentioning
confidence: 99%
“…More recently, Eggers, Holley, et al [5] used a point mass dynamic model connected to Monte Carlo simulation and achieved results similar to Macqueen and Ainsilie [3]. Montgomerie [6] expanded the work of others [2][3][4][5] by dynamically modeling fragments with a rigid 6 degree of freedom dynamic model representation. Very large throw distances are shown which fall out of the range of most other reported efforts.…”
Section: Introductionmentioning
confidence: 99%
“…Eggers et al reported on a fragment analysis of the NWTC in 2001. Although they made several parametric studies that may pave a path towards generalizing the problem, their overall model assumed a constant drag coefficient ( C D ) of 0.5, which would be considered high compared with findings from Sørensen and Larwood and van Dam .…”
Section: Introductionmentioning
confidence: 99%