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Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions
Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions
- Source :
- AIAA Journal. 59:140-149
- Publication Year :
- 2021
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2021.
-
Abstract
- An experimental investigation has been conducted on swept impinging oblique shock/boundary-layer interactions at a nominal Mach number of 2.28 with a fully turbulent incoming boundary layer (Reθ=55...
- Subjects :
- 020301 aerospace & aeronautics
Stagnation temperature
Materials science
Turbulence
Astrophysics::High Energy Astrophysical Phenomena
Aerospace Engineering
Boundary (topology)
02 engineering and technology
Mechanics
01 natural sciences
010305 fluids & plasmas
Physics::Fluid Dynamics
symbols.namesake
Boundary layer
0203 mechanical engineering
Particle image velocimetry
Mach number
Physics::Plasma Physics
0103 physical sciences
symbols
Swept wing
Oblique shock
Astrophysics::Earth and Planetary Astrophysics
Astrophysics::Galaxy Astrophysics
Subjects
Details
- ISSN :
- 1533385X and 00011452
- Volume :
- 59
- Database :
- OpenAIRE
- Journal :
- AIAA Journal
- Accession number :
- edsair.doi...........6df6fba59ff3f794482fe04cac0f30f3
- Full Text :
- https://doi.org/10.2514/1.j058910