Analysis and Evaluation of the Momentum Theory Errors as Applied to Propellers
Author:
Affiliation:
1. Università degli Studi di Napoli “Federico II,” 80125 Naples, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J055131
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1. Efficient method for calculating the axial velocities induced along rotating blades by trailing helical vortices
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5. Compressible Helicoidal Surface Theory for Propeller Aerodynamics and Noise
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