Side Gust Effects on the Performance of a Supersonic Inlet with Bleed
Abstract
A computational investigation on the effects of side gust on the performance of a supersonic inlet with a bleed system at Mach 1.8 is reported. This is an extension to a recent study (Halwas, H. K., and Aggarwal, S. K., “Effect of Side Gust on the Performance of External Compression Supersonic Inlet,” Journal of Aircraft, Vol. 56, No. 2, March 2019, pp. 569–582) that analyzed a similar inlet without bleed. The supersonic section is designed...
Paper Details
Title
Side Gust Effects on the Performance of a Supersonic Inlet with Bleed
Published Date
Nov 1, 2019
Journal
Volume
56
Issue
6
Pages
2357 - 2370
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