Thursday, June 30, 2011

National Advisory Committee for Aeronautics (NACA): A Rapid Approximate Method for the Design of Hub Shroud Profiles of Centrifugal Impellers of Given Blade Shape: March 1955

National Advisory Committee for Aeronautics (NACA): A Rapid Approximate Method for the Design of Hub Shroud Profiles of Centrifugal Impellers of Given Blade Shape: March 1955 Review


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National Advisory Committee for Aeronautics (NACA): A Rapid Approximate Method for the Design of Hub Shroud Profiles of Centrifugal Impellers of Given Blade Shape: March 1955 Feature


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Posted by Alen Akseli at 6:11 AM
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