Abstract
By considering Radon measure solutions for boundary value problems of stationary non-isentropic compressible Euler equations on hypersonic-limit flows passing ramps with frictions on their boundaries, we construct solutions with density containing Dirac measures supported on the boundaries of the ramps, which represent the infinite-thin shock layers under different assumptions on the skin-frictions. We thus derive corresponding generalizations of the celebrated Newton-Busemann law in hypersonic aerodynamics for distributions of drags/lifts on ramps.
| Original language | English |
|---|---|
| Journal | Acta Mathematicae Applicatae Sinica |
| DOIs | |
| State | Accepted/In press - 2024 |
Keywords
- 35L50
- 35L65
- 35Q31
- 35R06
- 76K05
- Dirac measure
- Newton-Busemann law
- Radon measure solution
- compressible Euler equations
- hypersonic-limit flow
- skin friction