This paper presents our design concept of a new rotor blade for an existing 300 kW WTGS with a horizontal axis rotor. This two-bladed WTGS is evaluated to have rather poor performance in terms of annual output due to the deficiencies in aerodynamic design of blade and its high noise emission level w
An engineering approximation for the aerodynamic loading of helicopter rotor blades
โ Scribed by M.I. Young
- Publisher
- Elsevier Science
- Year
- 1966
- Tongue
- English
- Weight
- 841 KB
- Volume
- 4
- Category
- Article
- ISSN
- 0022-460X
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