Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Community Noise
- 8 May 2006
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 2. Installed NozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 3. Jet-Flap InteractionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Computational Analysis of a Chevron Nozzle Uniquely Tailored for Propulsion Airframe AeroacousticsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Shockcell 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
- Jet-Pylon Interaction of High Bypass Ratio Separate Flow Nozzle ConfigurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2004
- Computational and Experimental Flowfield Analyses of Separate Flow Chevron Nozzles and Pylon InteractionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2003