NASA NTRS · 19710000152
Computer program for calculating aerodynamic forces on blade sections
Abstract
Calculation is taken from pressure or velocity distribution along blade surface. Blade sections have either one or two /tandem/ blade segments. Program is recommended primarily for use with ideal flow pressure distributions where forces in drag direction are neglected.
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Mcnally, W. D.. 1971-06-01. Computer program for calculating aerodynamic forces on blade sections. https://ntrs.nasa.gov/citations/19710000152
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