A submerged inlet investigation, using flow control in the form of
discrete blowing, examined proximity and jet directionality to
improve compressor face uniformity. The flow control locations were
at the head of the ramp and part way down the ramp, providing four
configurations under examination. Laser Doppler velocimetry
(LDV)measurements at the throat determined the effect of the flow
control based on the statistical velocity measurements. Blowing at
closer proximity to the throat and targeting the largest velocity
deficit region provided the best results. The airspeed and inlet
velocity simulated takeoff and landing conditions; velocities
ranged from Mach 0.1-0.3 at the throat. Secondary components and
turbulence measurements proved useful in determining the effect of
the flow control configurations.
General
| Imprint: |
Biblioscholar
|
| Country of origin: |
United States |
| Release date: |
October 2012 |
| First published: |
October 2012 |
| Authors: |
Tina Reynolds
|
| Dimensions: |
246 x 189 x 10mm (L x W x T) |
| Format: |
Paperback - Trade
|
| Pages: |
184 |
| ISBN-13: |
978-1-249-62504-9 |
| Categories: |
Books >
Social sciences >
Education >
General
|
| LSN: |
1-249-62504-1 |
| Barcode: |
9781249625049 |
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