NASA NTRS · 19820020428
Streamlining the walls of an empty two-dimensional flexible-walled test section
Abstract
The techniques used to find aerodynamically straight wall contours in a test section of a transonic wind tunnel are discussed. The walls were defined as aerodynamically straight up to Mach 0.9.
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Wolf, S. W. D., Goodyer, M. J., Cook, I. D.. 1982-05-01. Streamlining the walls of an empty two-dimensional flexible-walled test section. https://ntrs.nasa.gov/citations/19820020428
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