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Interactive 3D model of Scramjet Combustor with Regenerative Cooling

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Scramjet Combustor with Regenerative Cooling

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Bounding box
59.0 × 59.0 × 262.0 mm
Engine
Precision B-rep
Parameters
11
Published
September 23, 2026

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The prompt

Create a detailed parametric 3D CAD model of a scramjet combustor with regenerative cooling. Dimensions: - Combustor length: 250 mm - Internal diameter: 8.95 mm - Wall thickness: 20 mm - Cooling tube radius: 9 mm Design a hollow cylindrical combustor with a continuous internal hot-gas passage. Embed multiple evenly spaced helical cooling channels inside the combustor wall. The channels must follow the outer circumference and run along the full combustor length. Add coolant inlet and outlet manifolds connected to the cooling channels. Keep all cooling channels enclosed inside the wall and separated from the hot-gas passage. Make the geometry clean, fully parametric, manufacturable, and suitable for CFD, conjugate heat transfer, and FEA. Include inlet, outlet, hot-gas passage, cooling channels, coolant inlet and coolant outlet.

Parameters

NameValueRange
Combustor Length250 mm80 – 600
Hot-Gas Passage Diameter8.95 mm3 – 60
Wall Thickness20 mm4 – 60
Cooling Channel Radius9 mm1 – 9.5
Cooling Channel Count4 ea1 – 8
Helical Pitch40 mm20 – 260
Outer Skin Over Manifold3.5 mm1 – 8
Inner Rib (Manifold to Hot Gas)1 mm0.5 – 6
Manifold Axial Length12 mm4 – 40
End Cap Thickness3 mm2 – 20
Coolant Port Radius5 mm1 – 6

Every value above is a live dimension. Open a model like this in the editor and each one becomes a slider you can drag before exporting.

Scramjet Combustor with Regenerative Cooling - Free CAD Model (STEP, STL) | TextoCAD