Minimum swept-wing induced drag with constraints on lift and pitching moment.
Author:
Affiliation:
1. Douglas Aircraft Company, Inc., Long Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.43797
Reference3 articles.
1. Perkins, C. D. and Hage, R. E., Airplane Performance, Stability and Control (John Wiley & Sons, New York, 1949), pp.89-92.
2. Theory of Maxima and Minima
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