The generic models listed below are ENFLOW instantiations of the test cases described in the references.

RAE 2822 Airfoil

A test case commonly used to validate CFD method for transonic flow around a two-dimensional airfoil, defined by Royal Aeronautical Establishment.

LANN Wing

A test case commonly used to validate CFD method for unsteady transonic airfoil around an isolated wing, defined in a joint effort by Lockheed, Air Force, NASA and NLR.

DLR-F4 Wing/Body

A test case commonly used to validate CFD method for transonic flow around a wing/body aircraft configuration, also used for the 1st AIAA Drag Prediction Workshop I.

DLR-F6 Wing/Body/Nacelle

A test case commonly used to validate CFD method for transonic flow around a considerably complete aircraft configuration (Wing/Body/Nacelle), also used for the 2nd AIAA Drag Prediction Workshop II.

NASA Rotor 67

A test case commonly used to validate CFD method for transonic flow around a rotating fan representative for turbofan engine, defined by NASA.

VFE-2 Delta Wing

A test case commonly used to validate CFD method for vortical flow around a delta wing, defined in the framework of the 2nd International Vortex Flow Experiment.