Accession Number:

ADA014247

Title:

Investigation of Self-Induced Blowing and Suction Across a Region of Shock Wave-Boundary Layer Interaction.

Descriptive Note:

Interim rept. Mar-May 75,

Corporate Author:

AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1975-06-01

Pagination or Media Count:

16.0

Abstract:

Self-induced blowing and suction were used in an attempt to reduce the separated region of a shock-boundary layer interaction. High pressure air was channeled from the downstream side of the separated bubble to the low pressure boundary layer upstream of the interaction. Data obtained from the configurations tested in this study showed no improvement over the plain wall separation case. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE