Drag coefficients for partially inflated flat circular parachutes [PDF]
Free-body tests of flat circular parachutes and determination of aerodynamic drag coefficients during partial ...
Scher, S. H., Young, I. G.
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The control of wing kinematics and flight forces in fruit flies (Drosophila spp.) [PDF]
, 1998 By simultaneously measuring flight forces and stroke kinematics in several species of fruit flies in the genus Drosophila, we have investigated the relationship between wing motion and aerodynamic force production. We induced tethered flies to vary their
Dickinson, Michael H. +1 more
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Aerodynamic detuning analysis of an unstalled supersonic turbofan cascade [PDF]
An approach to passive flutter control is aerodynamic detuning, defined as designed passage-to-passage differences in the unsteady aerodynamic flow field of a rotor blade row.
Fleeter, S., Hoyniak, D.
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Application of a panel method to wake-vortex/wing interaction and comparison with experimental data [PDF]
The ability of the Vortex Separation AEROdynamics (VSAERO) program to calculate aerodynamic loads on wings due to interaction with free vortices was studied.
Ross, James C., Smith, Brian E.
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Aerodynamical Coefficients on Cambered Surfaces [PDF]
Aeronautical journal (London, England : 1897), 1912 openaire +1 more source
Uncertainty Analysis of the Aerodynamic Coefficients
, 2017 This thesis treats an error propagation analysis used to estimate the uncertainty of the aerodynamic coefficients. The propagation methods used in this analysis are a Taylor Series Method and a Monte Carlo Method. The Taylor Series Method uses the partial derivatives of each input variable whereas the Monte Carlo Method uses random and repeated samples
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Aerodynamic Coefficients of Stationary and Spinning Cricket Balls
, 2007 The flight of a cricket ball after leaving the hand of a bowler is, for given atmospheric conditions, principally governed by the speed of the ball, the angle of the seam to the direction of flight, any rotational spin applied to the ball, and the state of its outer surface with regard to the degree of wear and roughness.
Sayers, A.T., Lelimo, N.J.
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Correlation of SA349/2 helicopter flight-test data with a comprehensive rotorcraft model [PDF]
A comprehensive rotorcraft analysis model was used to predict blade aerodynamic and structural loads for comparison with flight test data. The data were obtained from an SA349/2 helicopter with an advanced geometry rotor.
codes., Yamauchi, Gloria K.
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Study of aerodynamic characteristics of variable cross-section box girders under three-dimensional fluctuating wind field. [PDF]
Sci RepFeng X, Jia J.
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Numerical investigation of co-flow jet integration to enhance the aerodynamic efficiency of airfoils used in wind turbine applications. [PDF]
Sci RepFarghaly MB +3 more
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