Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes-Reference-Cited by-同舟云学术

Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes

Published:2019-03 Issue:2 Volume:56 Page:405-420
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Radespiel Rolf,Ali Syed R. C.,Muñoz Federico,Bowersox Rodney,Leidy Andrew,Tanno Hideyuki¹,Kirk Lindsay C.²,Reshotko Eli³

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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