SimScale simulation projects by c_parker | Page 1

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A simulation of the NASA CRM with winglet placed at 105mm height, 50 degrees cant angle and -4 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 50 degrees cant angle and -3.5 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 50 degrees cant angle and -5 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 50 degrees cant angle and -4.5 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 50 degrees cant angle and -3 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 110mm height, 50 degrees cant angle and -4 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 52 degrees cant angle and -4 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 54 degrees cant angle and -4 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 48 degrees cant angle and -4 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 46 degrees cant angle and -4 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 95mm height, 50 degrees cant angle and -4 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 90mm height, 50 degrees cant angle and -4 degrees twist angle.

Final winglet design for the NASA CRM. An elliptical winglet of 110mm height, 48 degrees cant angle and -4.5 degrees twist angle attached to the wing tip of the NASA Common Research Model.

NASA CRM modified with an elliptical winglet at 70 degrees cant angle and 50mm in height.

A simulation of the NASA CRM with winglet placed at 100mm height, 70 degrees cant angle and +4 degrees twist angle.

A simulation of the NASA CRM with a winglet of 150mm height and 70 degrees cant angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 70 degrees cant angle and -4 degrees twist angle.

A second simulation of the NASA CRM after model has been scaled correctly.

A simulation of the NASA CRM with a winglet of 125mm height and 70 degrees cant angle.

A simulation of the NASA CRM with a winglet of 100mm height and 70 degrees cant angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 70 degrees cant angle and -2 degrees twist angle.

A simulation of the NASA CRM with a winglet of 75mm height and 70 degrees cant angle.

A simulation of the NASA CRM with winglet placed at 100mm height, 70 degrees cant angle and +2 degrees twist angle.

A simulation of the NASA CRM with winglet placed at 100mm height and 90 degrees cant angle.

A simulation of the NASA CRM with winglet placed at 100mm height and 50 degrees cant angle.

A simulation of the NASA CRM with winglet placed at 100mm height and 30 degrees cant angle.

The simulation that have been done by DR Sugar-Gabor. To look at for reference and to use as a guide for my simulation.

Tutorial project for a flow analysis of a pipe junction. The project only provides the geometry to start with. See our tutorials section to have a look at the step-by-step instructions to set up the simulation.

First attempt at simulating the flow around the CRM.

Meshing tutorial of flow through a pipe junction.

Tutorial project for setting up the Automated Hex-dominant for internal flow for an angled pipe geometry.

A simulation of the NASA CRM with winglet placed at 100mm height, 50 degrees cant angle and -4 degrees twist angle.

Sample project for how to set-up the Hex-Dominant Parametric mesh for flow around a vehicle body.

Tutorial: Incompressible turbulent airflow around a spoiler

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