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)
Year: 1990
Type: article
Source: Journal of Turbomachinery
DOI: 10.1115/1.2927641
Authors: W. C. Zierke, S. Deutsch
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W2061289891