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
A statistical model for landing gear noise prediction
โ Scribed by Yueping Guo
- Publisher
- Elsevier Science
- Year
- 2005
- Tongue
- English
- Weight
- 665 KB
- Volume
- 282
- Category
- Article
- ISSN
- 0022-460X
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