Wing design for minimum drag with practical constraints
Author:
Affiliation:
1. Simon Fraser University, Burnaby, British Columbia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45058
Reference11 articles.
1. Klein A and Viswanathan S P Approximate Solution for Minimum Induced Drag of Wings with Given Structural Weight Journal of Aircraft, Vol12Feb 1975pp124126
2. 5Lebert G ' Spanwise Lift Distribution of Forward and Aft Swept Wings in Comparison with the Optimum Distribution Form ' Journal of Aircraft Vol 18 Junel 981,pp 496-498
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