Published November 28, 2017
| Accepted Version
Conference Paper
Open
Studies of the large-scale structure in adiabatic and moderately-wall-heated subsonic boundary layers
Chicago
An error occurred while generating the citation.
Abstract
Simultaneous velocity-optical measurements in subsonic boundary layers were conducted in order to investigate the relationship between the instantaneous 2-D wavefronts, measured by different optical sensors, the Malley probe and 2-D Shack-Hartmann sensors, and the instantaneous large-scale structure along a wall-normal plane, using PIV in both incompressible and compressible subsonic boundary layers. These systematic studies of the instantaneous relation between the large-scale boundary layer structure and its aero-optical signature provide additional understanding of the instantaneous dynamics of the large-scale structure at subsonic and transonic speeds.
Additional Information
SESSION 7A - Wall Turbulence: Large Structures. The support of the Department of Defense through the National Defense Science & Engineering Graduate Fellowship (NDSEG) Program and the Air Force Office of Scientific Research Grant # FA9550-12-1-0060 are gratefully acknowledged. The U.S. Government is authorized to reproduce and distribute reprints for governmental purposes notwithstanding any copyright notation thereon.Attached Files
Accepted Version - 7A-3.pdf
Files
7A-3.pdf
Files
(645.9 kB)
| Name | Size | Download all |
|---|---|---|
|
md5:cec13fb08760d96c6ca1789b650b4d8f
|
645.9 kB | Preview Download |
Additional details
- Eprint ID
- 83521
- Resolver ID
- CaltechAUTHORS:20171128-113834714
- National Defense Science and Engineering Graduate (NDSEG) Fellowship
- Air Force Office of Scientific Research (AFOSR)
- FA9550-12-1-0060
- Created
-
2017-11-28Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- GALCIT