Aerodynamic performance effects due to small leading-edge ice (roughness) on wings and tails
Author:
Affiliation:
1. McDonnell Douglas Corporation, Long Beach, California 90846
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46420
Reference6 articles.
1. Calculation of incompressible rough-wall boundary-layer flows
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