Blade Element Rotor Theory
Book Details
Format
Paperback / Softback
ISBN-10
1032283041
ISBN-13
9781032283043
Publisher
Taylor & Francis Ltd
Imprint
CRC Press
Country of Manufacture
GB
Country of Publication
GB
Publication Date
Oct 8th, 2024
Print length
169 Pages
Weight
340 grams
Product Classification:
Applied mathematicsClassical mechanicsFluid mechanicsPhysics: Fluid mechanicsEngineering: generalMechanical engineeringMaterials scienceDynamics & vibrationEngineering: Mechanics of fluidsMechanics of fluidsPower generation & distributionEnergy, power generation, distribution and storageEnvironmental science, engineering & technologyEnvironmental science, engineering and technologyAerospace & aviation technologyAerospace and aviation technologyAstronautics
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Blade Element Rotor Theory presents an extension of the blade element rotor theory to describe the dynamic properties of helicopter rotors. It focuses on the more precise mathematical determination of the forces and moments by which a rotor affects its rotorcraft at specified flight conditions and control positions.
Blade Element Rotor Theory presents an extension of the blade element rotor theory to describe the dynamic properties of helicopter rotors. It focuses on the more precise mathematical determination of the forces and moments by which a rotor affects its rotorcraft at specified flight conditions and control positions.
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