Title: Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
Abstract: From Introduction: The present paper employs an approach believed to be novel in slender-body theory and is concerned with developing formulas for the forces and moments as well as the stability derivatives for general slender wing-body combinations.
Publication Year: 1954
Publication Date: 1954-11-01
Language: en
Type: article
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Cited By Count: 12
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