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Supersonic Cavity Flow Subjected to Continuous and Transient Leading-Edge Blowing
- Source :
- AIAA Journal. 58:4415-4425
- Publication Year :
- 2020
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2020.
-
Abstract
- A rectangular cavity (L/D=5.67) with Mach 1.5 freestream was subjected to a large temporal variation in leading-edge blowing in order to experimentally investigate the effect on aerodynamic and aer...
- Subjects :
- 020301 aerospace & aeronautics
Stagnation temperature
Leading edge
Materials science
Aerospace Engineering
Pressure-sensitive paint
02 engineering and technology
Aerodynamics
Mechanics
Boundary layer thickness
01 natural sciences
010305 fluids & plasmas
Physics::Fluid Dynamics
symbols.namesake
0203 mechanical engineering
Mach number
0103 physical sciences
symbols
Supersonic speed
Freestream
Subjects
Details
- ISSN :
- 1533385X and 00011452
- Volume :
- 58
- Database :
- OpenAIRE
- Journal :
- AIAA Journal
- Accession number :
- edsair.doi...........769bc236f657cb5f75117d1c76ff0275
- Full Text :
- https://doi.org/10.2514/1.j059267