SAE ARP265A

SAE ARP265A – Airfoil Shapes – Dimensioning of Turbine Engine

This Aeronautical Recommended Practice provides a standard method for locating and dimensioning the airfoil portions of parts such as blades and vanes. This method will apply to blades or vanes with or without a base. The forms of attachment are varied; therefore the blade bases shown in the following figures are for illustration only. All dimensions and notes shown pertaining to the common functional point line or plane are considered to be applied to a datum on or off the part irrespective of the form of attachment.

Product Details

Published:

02/01/1959

File Size:

1 file 120 KB

Note:

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