Winglet Toe-Out Angle Optimization for the Gates Learjet Longhorn Wing
- 1 December 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 17 (12) , 851-855
- https://doi.org/10.2514/3.57976
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Gates Learjet Model 28/29, the first 'Longhorn' LearjetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978