Annular Aerospike Plug Nozzle Axial Thrust & Throat Acceleration
Rocket Propulsion Aerodynamics (CFD)PASS · 1.07%Axial aerodynamic force, annular throat acceleration, and truncated base wake recirculation for an altitude-compensating annular aerospike plug nozzle with 6 cooling pylon struts.
- Tolerance:
- 5%
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Open & Solve in BrowserProblem statement
- Geometry
- Cylindrical test cell Ø210 × 420 mm containing a contoured central aerospike plug (Ø100 mm throat shoulder, two-stage ramp, Ø32 mm truncated base), outer cowling shroud (14 mm annular throat gap), and 6 pitched struts (12°).
- Material
- Air at 20 °C (rho = 1.204 kg/m³, mu = 1.825e-5 Pa·s).
- Boundary conditions
- Inlet velocity U = 50.0 m/s along +X, outlet gauge pressure 0 Pa, outer cylindrical boundary symmetry, aerospike plug, shroud, and 6 struts viscous no-slip walls.
- Measured quantity
- Total axial aerodynamic force Fx (target 5.55 kN from annular throat momentum theory, computed 5.49 kN) and peak jet velocity |U|_max = 313.96 m/s.
WebCAE Terminal
Paste these commands into the Terminal panel inside WebCAE. They use the same text DSL as the application; run one command per line:
units mm
import path="cfd_aerospike_plug_nozzle.step" format=step
mesh tet size=22
cfd fluid air
cfd set mode=steady speed=50.0 turbulence=sst iterations=200 tol=1e-4 threads=8 intensity=5 multigrid=0 cfl=4.0
cfd inlet surface number 3 speed=50.0 intensity=0.05
cfd outlet surface number 2 pressure=0
cfd symmetry surface number 1
cfd wall surface number 4 monitor=on
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solve cfdResults comparison
| Reference value | 5.55 kN |
| Our result | 5.49 kN |
| Deviation | 1.07% |
| Tolerance | 5% |
| Status | PASS · 1.07% |
| Element family | Finite-volume CFD |
| Mesh details | 2448 узлов, 8627 тет (Netgen P1 tet mesh, кольцевое клиновое сопло Aerospike + 6 пилонов) |
Updated: 2026-10-19 · WebCAE 0.2.0 · 54751b2e+dirty