Off-Design Performance of Wavecatcher Intakes Based on Intake Shapes

High-speed airbreathing vehicles operating in the hypersonic region are subjected to various flight conditions, making it essential to investigate their performance characteristics under off-design conditions. The wavecatcher intake, known for better performance than conventional two-dimensional intakes, has been widely studied. However, a systematic method for defining its inlet and outlet geometries is still lacking. This numerical study identifies key flow parameters to establish relationships between intake shape and flow characteristics. Based on these correlations, design strategies for inlet and outlet geometries are proposed to enhance off-design starting performance. Using computational fluid dynamics (CFD), three intake configurations were evaluated: rectangular-to-elliptical transition (REST), rectangular-to-rectangular (RtR), and a newly developed semicircular-to-elliptical transition (SEST). For REST and RtR, two aspect ratios were tested to examine their geometric influence. The design point was Mach 7 at 28.7 km altitude, and three-dimensional CFD analyses were conducted for off-design conditions, including angles of attack from [Formula: see text], freestream Mach numbers from 5 to 10, and sideslip angles from 2 to 10 deg. The results show that the SEST configuration provides robust starting performance across all off-design conditions, making it a highly effective option for wavecatcher intake design.

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Publication Details

Journal
Journal of Aircraft
Published
2026-10-05
DOI
https://doi.org/10.2514/1.c038855
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
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article

Off-Design Performance of Wavecatcher Intakes Based on Intake Shapes

Sangyoon Lee, Hyoung Jin Lee, Young Jin Kim
Journal of Aircraft
Computational Fluid Dynamics and Aerodynamics
article

Off-Design Performance of Wavecatcher Intakes Based on Intake Shapes

Sangyoon Lee, Hyoung Jin Lee, Young Jin Kim
article en

Abstract

High-speed airbreathing vehicles operating in the hypersonic region are subjected to various flight conditions, making it essential to investigate their performance characteristics under off-design conditions. The wavecatcher intake, known for better performance than conventional two-dimensional intakes, has been widely studied. However, a systematic method for defining its inlet and outlet geometries is still lacking. This numerical study identifies key flow parameters to establish relationships between intake shape and flow characteristics. Based on these correlations, design strategies for inlet and outlet geometries are proposed to enhance off-design starting performance. Using computational fluid dynamics (CFD), three intake configurations were evaluated: rectangular-to-elliptical transition (REST), rectangular-to-rectangular (RtR), and a newly developed semicircular-to-elliptical transition (SEST). For REST and RtR, two aspect ratios were tested to examine their geometric influence. The design point was Mach 7 at 28.7 km altitude, and three-dimensional CFD analyses were conducted for off-design conditions, including angles of attack from [Formula: see text], freestream Mach numbers from 5 to 10, and sideslip angles from 2 to 10 deg. The results show that the SEST configuration provides robust starting performance across all off-design conditions, making it a highly effective option for wavecatcher intake design.

Journal of Aircraft
Inha University (KR)
Openalex Percentile: Top 17%
Computational Fluid Dynamics and Aerodynamics
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Off-Design Performance of Wavecatcher Intakes Based on Intake Shapes — Sangyoon Lee, Hyoung Jin Lee, et al. · Journal of Aircraft (2026) | TGRS Research Map | TGRS