Development Of The USM Wind Tunnel Validation Model For Calibration by Sim, Chiow Moon

“…The experiment was conducted under incompressible flow. Pressure distribution at various angles of attack were measured and lift contribution was computed for the model. …”
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Study Of Aerodynamic Performances Of Gliders Using Computational Fluid Dynamics Analysis by Mustapa, Nabila

“…In this project, the flow is assumed to be laminar at steady state (gliding phase) with incompressible flow. Since the gliding altitude does not exceed 10 meters, the boundary condition which includes inlet and outlet pressure, temperature, and density can be assumed to be the same as at sea-level. …”
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