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Composite landing gear for F-16


Book ID
117205118
Publisher
Elsevier Science
Year
2003
Tongue
English
Weight
96 KB
Volume
47
Category
Article
ISSN
0034-3617

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This paper follows the general formulation of aircraft landing gear noise prediction to develop a component-based model, incorporating scaling laws of the theory of aerodynamic noise generation and correlations of these scaling laws with currently available test data. The method decomposes the landi