Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 2. Installed Nozzles
- 8 May 2006
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Community NoisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated NozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006