Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes
Author:
Affiliation:
1. JAXA Kakuda Space Center, Kakuda 9811525 Japan
2. NASA Johnson Space Center, Houston, Texas 77058
3. Case Western Reserve University, Cleveland, Ohio 44106
Funder
EOARD
Deutsche Forschungsgemeinschaft, DFG
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34295
Reference35 articles.
1. Aeroheating Testing and Predictions for Project Orion Crew Exploration Vehicle
2. Investigation of Hypersonic Laminar Heating Augmentation in the Stagnation Region
3. AliS. R. C.RadespielR.TheissA. “Transition Experiment with a Blunt Apollo Shape Like Capsule in Hypersonic Ludwieg Tube,” Deutscher Luft- und Raumfahrtkongress, DGLR Paper 2014-340270, 2014.
4. Protuberance Boundary Layer Transition for Project Orion Crew Entry Vehicle
5. Wake flow instability studies behind discrete roughness elements on a generic re-entry capsule
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