Sensing and Active Flow Control for Advanced Bwb Propulsion-Airframe Integration Concepts
- Indbinding:
- Paperback
- Sideantal:
- 150
- Udgivet:
- 29. juli 2013
- Størrelse:
- 189x246x8 mm.
- Vægt:
- 281 g.
- 2-3 uger.
- 26. november 2024
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- 1 valgfrit digitalt ugeblad
- 20 timers lytning og læsning
- Adgang til 70.000+ titler
- Ingen binding
Abonnementet koster 75 kr./md.
Ingen binding og kan opsiges når som helst.
Beskrivelse af Sensing and Active Flow Control for Advanced Bwb Propulsion-Airframe Integration Concepts
In order to realize the substantial performance benefits of serpentine boundary layer ingesting diffusers, this study investigated the use of enabling flow control methods to reduce engine-face flow distortion. Computational methods and novel flow control modeling techniques were utilized that allowed for rapid, accurate analysis of flow control geometries. Results were validated experimentally using the Techsburg Ejector-based wind tunnel facility; this facility is capable of simulating the high-altitude, high subsonic Mach number conditions representative of BWB cruise conditions.
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