Use of a wake-integral method for computational drag analysis
Author:
Affiliation:
1. Mississippi State University/National Science Foundation Engineering Research Center for Computational Field Simulation, Mississippi State, Mississippi 39762-6176
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13040
Reference7 articles.
1. Computational analysis of methods for reduction of induced drag
2. A generalized wake-integral approach for drag determination in three-dimensional flows
3. Drag calculations of wings using Euler methods
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