Simultaneous PIV and PLIF Imaging of Low-Temperature Ablation in a Mach 5 Turbulent Boundary Layer
Author:
Affiliation:
1. University of Texas, Austin
2. The University of Texas at Austin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-440
Reference25 articles.
1. Aerothermodynamics of the Stardust Sample Return Capsule
2. H. Otsu, K. Suzuki, K. Fujita, and T. Abe. Effect of ablative gas on the radiative environment around the MUSES-C reentry capsule. AIAA paper 99-3463.
3. Aerothermodynamic Analysis of Stardust Sample Return Capsule with Coupled Radiation and Ablation
4. Ablation Studies for a Super-Orbital Reentry Capsule Using a Three-Temperature Model
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1. Simultaneous Scalar and Velocity Imaging in a Mach Five Boundary Layer;AIAA Journal;2019-11
2. Heat-Shield Ablation Visualized Using Naphthalene Planar Laser-Induced Fluorescence;Journal of Spacecraft and Rockets;2017-03
3. Technique for studying ablation-products transport in supersonic boundary layers by using PLIF of naphthalene;Experiments in Fluids;2016-05
4. Simultaneous Measurements of Scalar and Velocity in a Mach 5 Turbulent Boundary Layer using Naphthalene PLIF and PIV;54th AIAA Aerospace Sciences Meeting;2016-01-02
5. Measurements of Ablation-Products Transport in a Mach 5 Turbulent Boundary Layer using Naphthalene PLIF;53rd AIAA Aerospace Sciences Meeting;2015-01-03
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