NASA NTRS ยท 19820008927
Analytical study of twin-jet shielding
Abstract
Progress in the refinement and evaluation of an analytical jet shielding model are summarized. The model consists of a point noise source impinging on a cylinder of heated flow in which the temperature and velocity are uniform across the cross section of the jet. The shielding jet is infinite in extent along the jet axis and the radius of the jet is constant. The analytical model was compared to experimental data for a point noise source impinging on an ambient temperature, subsonic jet and on a subsonic simulated hot jet using helium as the flow medium. Results of these comparisons are discussed.
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Gerhold, C. H.. 1982-01-01. Analytical study of twin-jet shielding. https://ntrs.nasa.gov/citations/19820008927
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