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Flow Control for a Submerged Inlet
Journal of Fluids Engineering, 2022Abstract Submerged inlets have the advantages of low drag, clean outer profile, and excellent stealth performance. Previous studies indicate that the zones of large total-pressure loss, located at the bottom and top regions of the exit plane, are the main cause of the poor aerodynamic performance in a submerged inlet.
Wenzhong Xie +3 more
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Flow structure of the ridge integrated submerged inlet
Aerospace Science and Technology, 2021Abstract Control of the boundary layer upstream and in the region of the engine inlet is an important consideration for airplane designers. One important aspect of this problem can be seen in the performance analysis of submerged inlets for which the design is based on boundary layer ingestion.
Eiman B Saheby +2 more
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Flowfield of a helicopter submerged inlet with power output shaft
Acta Mechanica Sinica/Lixue Xuebao, 2021zbMATH Open Web Interface contents unavailable due to conflicting licenses.
He-Xia Huang +2 more
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Effects of forebody boundary layer on the performance of a submerged inlet
The Aeronautical Journal, 2021ABSTRACTThe use of a submerged inlet is advantageous in modern aircrafts because of its low drag resistance, small radar cross section and ease of maintenance. Although it is well known that the forebody boundary layer deteriorates the aerodynamic performance of a submerged inlet, the level of impact has not yet been fully quantified.
W.Z. Xie +6 more
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MHD flow of submerged jets behind the inlet disturbance
PAMM, 2023AbstractIn a broad variety of configurations in technology and industrial applications, the properties of liquid metal flows subjected to strong magnetic fields, are largely governed by the dynamics of coherent structures, known to settle several basic types, such as thin shear layers, forming near the walls or within the fluid domain, vortices ...
Krasnov, Dmitry +5 more
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Design of S-Shaped Submerged Inlet
Advanced Materials Research, 2011The influence of centerline and the cross-section variation to aerodynamic performance of the inlet was researched in a wider range. A new method of measuring the total pressure recovery coefficient and total pressure distortion coefficient of the inlet was proposed.
Xiao Lin Li
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