Rough-Wall Heat Flux Augmentation Analysis Within the ExoMars Project
Author:
Affiliation:
1. DLR, German Aerospace Center, 51147 Cologne, Germany
2. Fluid Gravity Engineering, Ltd., Emsworth, England PO10 7BT, United Kingdom
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.A33306
Reference37 articles.
1. Aerothermodynamic Design of the Mars Science Laboratory Heatshield
2. Modification of the van Driest damping function to include the effects of surface roughness
3. NikuradseJ. “Law of Flow in Rough Pipes,” NACA TM-1292, 1933;
4. A model for rough wall turbulent heating and skin friction
5. ErdemE.MarianiR.KontisK. “Wind Tunnel Experiments on Roughness,” Univ. of Manchester, TR EXM-DM-TRP-MAN-0001, Manchester, England, U.K. 2011.
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