Evaluation of Skin Friction Drag for Liner Applications in Aircraft
Author:
Affiliation:
1. National Institute of Aerospace
2. NASA Langley Research Center
3. University of Notre Dame
Publisher
American Institute of Aeronautics and Astronautics
Reference22 articles.
1. DRE-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers
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4. Roberts, D.W. "Equivalent Sand-Grain Roughness of Perforated Plate Acoustic Linings," AIAA-P-77-104,
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