42,11 €
46,79 €
-10% with code: EXTRA
Sensing and Active Flow Control for Advanced Bwb Propulsion-Airframe Integration Concepts
Sensing and Active Flow Control for Advanced Bwb Propulsion-Airframe Integration Concepts
42,11
46,79 €
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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 hi…
46.79
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  • ISBN-10: 1289250405
  • ISBN-13: 9781289250409
  • Format: 18.9 x 24.6 x 0.8 cm, minkšti viršeliai
  • Language: English
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Sensing and Active Flow Control for Advanced Bwb Propulsion-Airframe Integration Concepts (e-book) (used book) | bookbook.eu

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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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  • Author: John Fleming
  • Publisher:
  • ISBN-10: 1289250405
  • ISBN-13: 9781289250409
  • Format: 18.9 x 24.6 x 0.8 cm, minkšti viršeliai
  • Language: English English

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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