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- Title
Some hypersonic intake studies.
- Authors
Lanson, F.; Stollery, J. L.
- Abstract
The article focuses on a study that analyzes a two-dimensional air intake flow starting process of a rocket comprising a wedge followed by an isentropic compression in the Cranfield Gun Tunnel at Mach 8-2. The effects of the cowl position, Reynolds number, boundary layer trip and introduction of a small restriction in the intake duct were analyzed. Experimental data gathered have showed good qualitative agreement intake flow process in multiple changes of parameters analyzed.
- Subjects
RAMJET rocket engine air intakes; REYNOLDS number; LAMINAR boundary layer; BOUNDARY layer (Aerodynamics); FLUID dynamics; AERODYNAMICS
- Publication
Aeronautical Journal, 2006, Vol 110, Issue 1105, p145
- ISSN
0001-9240
- Publication type
Article
- DOI
10.1017/S0001924000001123