Abstract
A numerical code has been developed to calculate the flowfield in two-dimensional high-speed inlets using the Navier-Stokes equations. Arbitrary inlet geometries may be specified, with variable bleed on the ramp and cowl surfaces. Turbulence is incorporated through an algebraic turbulent eddy viscosity. The code has been applied to the calculation of the flow in a simulated high speed inlet for two different bleed schedules.
| Original language | English (US) |
|---|---|
| Journal | AIAA Paper |
| State | Published - Jan 1 1980 |
| Event | AIAA Pap AIAA/SAE/ASME Jt Propul Conf, 16th - Hartford, CT, USA Duration: Jun 30 1980 → Jul 2 1980 |
All Science Journal Classification (ASJC) codes
- Engineering(all)