| Type of Document |
Master's Thesis |
| Author |
Henry, Michael Maier
|
| URN |
etd-01132002-212222 |
| Title |
Two-Dimensional Shock Sensitivity Analysis for Transonic Airfoils with Leading-edge and Trailing-edge Device Deflections |
| Degree |
Master of Engineering |
| Department |
Aerospace and Ocean Engineering |
| Advisory Committee |
| Advisor Name |
Title |
| Mason, William H. |
Committee Chair |
| Grossman, Bernard M. |
Committee Member |
| Schetz, Joseph A. |
Committee Member |
|
| Keywords |
- 2-D flow separation
- device deflection
- transonic airfoil
- shock movement
|
| Date of Defense |
2001-08-03 |
| Availability |
unrestricted |
Abstract
This investigation, in consideration of the sudden separation increase involved in wing drop, was to determine if the incorporated 2-D airfoil exhibits abnormal shock sensitivity. A comparative airfoil study was used to determine if this particular transonic airfoil is prone to abrupt shock movement, resulting in increased regions of separation.
|
| Files |
| Filename |
Size |
Approximate Download Time
(Hours:Minutes:Seconds)
|
| 28.8 Modem |
56K Modem |
ISDN (64 Kb) |
ISDN (128 Kb) |
Higher-speed Access |
| |
Henrysthesis.pdf |
478.54 Kb |
00:02:12 |
00:01:08 |
00:00:59 |
00:00:29 |
00:00:02 |
|
