Abstract
Mack-mode waves are measured in a hypersonic boundary layer using high-frequency focusing schlieren deflectometry. Experiments are performed using a flared cone at angle of attack in the low-disturbance Mach 6 Quiet Tunnel at Texas A&M University across a free-stream unit Reynolds number range of. The high-frequency response of the measurement system allows harmonics and other nonlinear behaviour to be measured. Mack-mode waves and several harmonics are clearly observed at a frequency of. Bispectral analysis is used to show that these waves undergo several quadratic phase-coupled sum and difference interactions with themselves to produce harmonics, as well interact with a relatively low-frequency wave that results in amplitude modulation. Bispectral analysis is used to highlight these interactions.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 74-99 |
| Number of pages | 26 |
| Journal | Journal of Fluid Mechanics |
| Volume | 872 |
| DOIs | |
| State | Published - Aug 10 2019 |
Keywords
- boundary layer stability
- high-speed flow
- nonlinear instability
ASJC Scopus subject areas
- Condensed Matter Physics
- Mechanics of Materials
- Mechanical Engineering
- Applied Mathematics