Accession Number:

AD1053910

Title:

An investigation of physics and control of flow passing a NACA0015 in fully reversed condition

Descriptive Note:

Technical Report

Corporate Author:

Ohio State University Columbus United States

Personal Author(s):

Report Date:

2015-12-06

Pagination or Media Count:

101.0

Abstract:

Flow control experiments were performed on a NACA 0015 airfoil in fully-reversed condition, which is anticipated to occur on the retreating blade side of advancedhelicopters such as slowed-rotor compound rotorcraft. Control was achieved using nanosecond dielectric barrier discharge NS-DBD plasma actuators.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE