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


See more picture


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


Check price now


Rerate Products


Customer Review

No comments:

Post a Comment