On the calculation of some two-dimensional inviscid jets
Abstract
Vorticity panel methods are applied to solve the interacting flow between an outer stream and a two-dimensional jet exhausting into that stream; both are assumed to be at low speed. The cases include a jet emerging from a thick afterbody and an inclined jet. The work is intended as a prelude to obtaining initial values for calculating the mixing of a jet with an outer stream.
- Publication:
-
Aeronautical Journal
- Pub Date:
- April 1984
- Bibcode:
- 1984AeJ....88..141S
- Keywords:
-
- Inviscid Flow;
- Panel Method (Fluid Dynamics);
- Two Dimensional Jets;
- Vorticity;
- Afterbodies;
- Interactional Aerodynamics;
- Jet Mixing Flow;
- Nozzle Flow;
- Fluid Mechanics and Heat Transfer