REDUCTION OF UNSTEADY STATOR–ROTOR INTERACTION USING TRAILING EDGE BLOWING-Reference-Cited by-同舟云学术

REDUCTION OF UNSTEADY STATOR–ROTOR INTERACTION USING TRAILING EDGE BLOWING

Published:2000-08 Issue:2 Volume:235 Page:235-245
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

LEITCH THOMAS A.,SAUNDERS C.A.,NG W.F.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference11 articles.

1. D. G. DUNN, N. A. PEART, 1973, NASA CR-114649, Aircraft noise source and contour estimation

2. I. A. WAITZ, J. M. BROOKFIELD, J. SELL, B. J. HAYDEN, 1995, First Joint CEAS/AIAA Aeroacoustics Conference, Munich, Germany, Preliminary assessment of wake management strategies for reduction of turbomachinery fan noise

3. The effects of jet injection geometry on two-dimensional momentumless wakes;PARK;Journal of Fluid Mechanics,1991

4. Suppression of the wake of a finite airfoil by trailing-edge blowing;MEYER;Bulletin of the American Physical Society,1991

5. Control of the wake from a simulated blade by trailing edge blowing;CORCORAN,1991

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