Wake Integration for Three-Dimensional Flowfield Computations: Applications
Author:
Affiliation:
1. Aircraft Research Association, Bedford MK41 7PF, England, United Kingdom
2. California Polytechnic State University, San Luis Obispo, California 93407
3. Oxford University, Oxford OX1 3QD, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2466
Reference17 articles.
1. Wake Integration for Three-Dimensional Flowfield Computations: Theoretical Development
2. Analysis of the elements of drag in three-dimensional viscous and inviscid flows
3. Determination of drag from three-dimensional viscous and inviscid flowfield computations
4. ACCURATE DRAG PREDICTION - A PREREQUISITE FOR DRAG REDUCTION RESEARCH
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