Accession Number:

AD0852524

Title:

Evolution of the Turbulence Wakes Behind Inlet Guide Vanes,

Personal Author(s):

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Report Date:

1968-12-18

Abstract:

Experimental results obtained from turbine exit cascades were studied to determine their applicability as compressor inlet guide vanes. The experimental investigations included wind tunnel studies at M 0.12 in which the inlet turbulence intensity was determined. Author

Supplementary Note:

Edited trans. of C M P-Cieplne Maszyny przeplywowe (Poland) n1 p213-220 1967.

Pages:

0014

Descriptors:

Identifiers:

Subject Categories:

File Size:

0.00MB

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