Low-speed aerodynamic characteristics of airfoil sections with rounded trailing edges in forward and reverse flow / by William D. Beasley and Robert J. McGhee.
|Main Author:||Beasley, William D.|
|Other Authors:||McGhee, Robert J.|
Washington, D.C. : National Aeronautics and Space Administration ; 1974.
Rotors (Helicopters) > Testing.
Wind tunnel tests.
Two dimensional flow.
"NASA TM X-3060."
Performing organization report no.: L-9327.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 9/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740025317_1974025317.pdf.
102 p. :
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