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Mode Behavior in Supersonic Cavity Flows
- Source :
- AIAA Journal. 57:3410-3421
- Publication Year :
- 2019
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2019.
-
Abstract
- The behavior of oscillation modes in a supersonic flow of a Mach number of 1.58 over a cavity of L/D=2 and L/W=0.89 was studied using wind-tunnel experiments. Through instantaneous shadowgraph visu...
- Subjects :
- Physics
020301 aerospace & aeronautics
Oscillation
Aerospace Engineering
02 engineering and technology
Mechanics
Boundary layer thickness
01 natural sciences
Compressible flow
010305 fluids & plasmas
Physics::Fluid Dynamics
symbols.namesake
0203 mechanical engineering
Mach number
0103 physical sciences
symbols
Shadowgraph
Supersonic speed
Astrophysics::Earth and Planetary Astrophysics
Choked flow
Wind tunnel
Subjects
Details
- ISSN :
- 1533385X and 00011452
- Volume :
- 57
- Database :
- OpenAIRE
- Journal :
- AIAA Journal
- Accession number :
- edsair.doi...........3f8de72fac52a449b6fce1990af06b0e
- Full Text :
- https://doi.org/10.2514/1.j057818