NASA NTRS · 19800046839
Some observations on supersonic wing design
Abstract
The paper presents a brief review on the development of supersonic wing design. Attention is given to linearized aerodynamic theory, emphasizing equations for drag and ratios of slopes and Mach lines. Diagrams that depict conditions for minimum drag as well as the effects of fore-and-aft dimension of wings and Mach numbers on areas of lateral entrainment are presented.
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Jones, R. T.. 1980-01-01. Some observations on supersonic wing design. https://ntrs.nasa.gov/citations/19800046839
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