STRUCTURAL - ACOUSTIC OPTIMIZATION OF SOUND TRANSMISSION INTO AND THROUGH AIRFRAME PANELS EXCITED BY TURBULENT BOUNDARY LAYERS

Project: Research project

Project Details

Description

IN THIS RESEARCH STRUCTURAL-ACOUSTIC OPTIMIZATION WILL BE APPLIED TO AIRCRAFT PANELS TO REDUCE INTERIOR NOISE. TURBULENT BOUNDARY LAYER FORCING FUNC

StatusFinished
Effective start/end date7/1/106/30/11

Funding

  • Langley Research Center: $30,000.00

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