Computational Analysis of a Chevron Nozzle Uniquely Tailored for Propulsion Airframe Aeroacoustics
- 8 May 2006
- proceedings article
- 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
- 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
- Computational Analysis of the Flow and Acoustic Effects of Jet-Pylon InteractionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
- Computational analysis of a pylon-chevron core nozzle interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2001
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