Winglet Toe-Out Angle Optimization for the Gates Learjet...

Winglet Toe-Out Angle Optimization for the Gates Learjet Longhorn Wing

Conley, Norm
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Volume:
17
Language:
english
Journal:
Journal of Aircraft
DOI:
10.2514/3.57976
Date:
December, 1980
File:
PDF, 1.27 MB
english, 1980
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