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Flow and Force Characteristics of 2-Percent-Thick Airfoils at Transonic Speeds
"A two-dimensional investigation utilizing pressure-distribution measurements and schileren photographs has been made of the flow and force characteristics of slab-sided airfoils of 2-percent thickness at transonic Mach numbers. The airfoils had various combinations of elliptically shaped leading and trailing edges from a fineness ratio of 0 to 10. The aerodynamic characteristics and an analysis of the flow past the models are presented" (p. 1).
Date:
January 18, 1955
Creator:
Lindsey, Walter F. & Landrum, Emma Jean
System:
The UNT Digital Library