An experimental documentation of trailing-edge flows at high Reynolds number [PDF]
Experiments documenting attached trailing-edge and near-wake flows at high Reynolds numbers are described. A long, airfoil-like model was tested at subsonic and low transonic Mach numbers, and both symmetrical and asymmetrical flows with pressure ...
Cleary, J. W. +2 more
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An aerodynamic analysis computer program and design notes for low speed wing flap systems [PDF]
The expanded capabilities for analysis and design of low speed flap systems afforded by recent modifications of an existing computer program is described.
Carlson, H. W., Walkley, K. B.
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Helicopter rotor trailing edge noise [PDF]
A two dimensional section of a helicopter main rotor blade was tested in an acoustic wind tunnel at close to full-scale Reynolds numbers to obtain boundary layer data and acoustic data for use in developing an acoustic scaling law and testing a first ...
Amier, R. K., Schlinker, R. H.
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Effect of blade trailing edge treatment on the hemolysis and hydraulic performance of left ventricular assist device. [PDF]
iScienceLai F, Cao C, Li Y, Qiu Z, Chen L.
europepmc +1 more source
Detection of Trailing Edge of Calcified Nodule After Rotational Atherectomy Using Optical Frequency Domain Imaging. [PDF]
CJC Open, 2019 Shiraishi J +3 more
europepmc +1 more source
Experimental analyses of trailing edge flows [PDF]
An experimental study of several of the trailing edge and wake turbulence properties for a NACA 64A010 airfoil section was completed. The experiment was conducted at the Ohio State University Aeronautical and Astronautical Research Laboratory in the 6 ...
Emmer, D. S., Petrie, S. L.
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Enhancing vehicle performance through the application of airfoils as spoilers with movable trailing edge. [PDF]
F1000ResKaraki A +3 more
europepmc +1 more source
Experimental investigation of trailing edge noise from stationary and rotating airfoils. [PDF]
J Acoust Soc Am, 2017 Zajamsek B +4 more
europepmc +1 more source
Wind tunnel evaluation of a truncated NACA 64-621 airfoil for wind turbine applications [PDF]
An experimental program to measure the aerodynamic performance of a NACA 64-621 airfoil with a truncated trailing edge for wind turbine applications has been conducted in the Ohio State University Aeronautical and Astronautical Research Laboratory 6 in ...
Gregorek, G. M., Law, S. P.
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Understanding the margin squeeze: Differentiation in fitness-related traits between central and trailing edge populations of Corallina officinalis. [PDF]
Ecol Evol, 2019 Kolzenburg R +5 more
europepmc +1 more source