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[American Institute of Aeronautics and Astronautics 23rd AIAA Applied Aerodynamics Conference - Toronto, Ontario, Canada ()] 23rd AIAA Applied Aerodynamics Conference - Finite Wing Lift-Curve Slope Calculations Using Lifting-Line Theory

โœ Scribed by Bridges, David


Book ID
121059601
Publisher
American Institute of Aeronautics and Astronautics
Year
2005
Weight
248 KB
Category
Article
ISBN
1624100589

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