Approximate solution of minimum induced drag of wings with given structural weight
- 1 February 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 12 (2), 124-126
- https://doi.org/10.2514/3.44425
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Minimum induced drag of wings with given lift and root-bending momentZeitschrift für angewandte Mathematik und Physik, 1973
- Federal Aviation Administration full-scale aircraft vortex wake turbulence flight test investigations - Past, present, futurePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971