Users of this system, can login to view this document.

Login

Enter the following information to request a copy of the document from the responsible person.

Closure to “Discussion of ‘The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees’” (1990, ASME J. Turbomach., 112, p. 255)

This email address is used for sending the document.