Publisher
American Institute of Aeronautics and Astronautics
Reference32 articles.
1. Study Type M∞ δ99=R Boundary Layer Beresh et al.20Exp. 1.5, 2.0 0.49, 0.41 Turbulent Morgan et al.19CFD 2.0 ∼0.20 Turbulent Morgan et al.18CFD 2.0 ∼0.25 Turbulent Wang et al.17Exp. 2.68 0.40 Turbulent Bathel et al.16Exp. & CFD 2.0 ∼1.25 Laminar Bernardini et al.15CFD 1.1-6.0 0.15-0.70 Laminar Iyer & Mahesh14CFD 3.37-8.23 0.15-0.70 Laminar Iyer et al.13CFD 3.37 0.13 Laminar Iyer et al.12CFD 3.37-8.23 0.64-2.54 Laminar Tirtey et al.12Exp. & CFD 6.0 0.94-2.01 Laminar Iyer et al.10CFD 3.37-8.23 0.64-2.54 Laminar Danehy et al.9Exp. 3.37-8.28 1.25 Laminar
2. Application of fast-responding pressure-sensitive paint to a hemispherical dome in unsteady transonic flow
3. Density Measurements of a Turbulent Wake Using Acetone Planar Laser-Induced Fluorescence
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