Flight Test Results for Uniquely Tailored Propulsion Airframe Aeroacoustic Chevrons: Shockcell Noise
- 8 May 2006
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- The Quiet Technology Demonstrator Program: Flight Validation of Airplane Noise-Reduction ConceptsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- 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: 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
- Effect of Uniform Chevrons on Cruise Shockcell NoisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Acoustic and Flow-Field Characteristics of Shock-cell Noise from Dual Flow NozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
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