NASA NTRS · 19980227969
Two-Dimensional, Supersonic, Linearized Flow with Heat Addition
Abstract
Calculations are presented for the forces on a thin supersonic wing underneath which the air is heated. The analysis is limited principally to linearized theory but nonlinear effects are considered. It is shown that significant advantages to external heating would exist if the heat were added well below and ahead of the wing.
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Lomax, Harvard. 1959-02-01. Two-Dimensional, Supersonic, Linearized Flow with Heat Addition. https://ntrs.nasa.gov/citations/19980227969
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