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NASA NTRS ยท 19810064683

Forebody drag reduction

Abstract

It is shown that the mechanisms of forebody drag reduction by means of either a spike or a forward-facing jet are similar, with the maximum achievable drag reduction being of the same order. Because the jet may be a relatively cool gas, however, the forward facing jet has the additional capability of reducing the aerodynamic heating that is so severe at high Mach numbers. By means of the correlation presented, jet ejection parameters may be chosen to achieve maximum permissible forebody drag reduction. The correlation method uses a momentum coefficient that characterizes jet efflux and freestream conditions.

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BibTeXRIS

Pamadi, B. N.. 1981-10-01. Forebody drag reduction. https://ntrs.nasa.gov/citations/19810064683

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