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- Publisher
- Springer Journals
- Copyright
- Copyright © I.I. Mazhul and Yu.P. Gounko 2022
- ISSN
- 0869-8643
- eISSN
- 1531-8699
- DOI
- 10.1134/s0869864322040035
- Publisher site
- See Article on Publisher Site
Abstract
The paper presents the results of a numerical simulation of conditions for starting a supersonic air intake using the bypass of part of the captured air through longitudinal slots. The air-intake duct consists of a narrowing entrance section and a constant-cross-section throat, both elements being constructed using flat surfaces, and the air intake contains longitudinal slots stretching along the lower flat surface. Various variants of the sectional bleeding of air are investigated, and changes in the flow structure in the intake duct depending on the air bleeding variant are demonstrated. Numerical modeling of the three-dimensional flow was performed for free-stream Mach number M∞ = 4 on the basis of Reynolds-averaged Navier-Stokes equations and the k−ω SST model of turbulence.
Journal
Thermophysics and Aeromechanics – Springer Journals
Published: Jul 1, 2022
Keywords: numerical simulation; supersonic flow; longitudinal slots; air bypass; air-intake start