NASA NTRS · 19730044026
Transonic flow about lifting configurations.
Abstract
A transonic flow solution is presented for configurations with span-to-length ratios of order one. The angles of attack are sufficiently large to produce lift effects that are either dominant or comparable to the thickness effects. The analysis is performed with the aid of the method of matched asymptotic expansions. The results obtained are compared with data reported by Cheng and Hafez (1972).
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Barnwell, R. W.. 1973-05-01. Transonic flow about lifting configurations.. https://ntrs.nasa.gov/citations/19730044026
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