2006
DOI: 10.2514/1.12225
|View full text |Cite
|
Sign up to set email alerts
|

Active Control of Separation from the Flap of a Supercritical Airfoil

Abstract: Active flow control in the form of periodic zero-mass-flux excitation was applied at several regions on the leading edge and trailing edge flaps of a simplified high-lift system t o delay flow separation. The NASA Energy Efficient Transport (EET) supercritical airfoil was equipped with a 15% chord simply hinged leading edge flap and a 25% chord simply hinged trailing edge flap. Detailed flow features were measured in an attempt to identify optimal actuator placement. The measurements included steady and unstea… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1

Citation Types

3
40
0
1

Year Published

2007
2007
2018
2018

Publication Types

Select...
5
2
1

Relationship

0
8

Authors

Journals

citations
Cited by 68 publications
(44 citation statements)
references
References 8 publications
3
40
0
1
Order By: Relevance
“…The low Reynolds number SHL results on the BART model 2,3 indicated that the momentum required to control flow separation on the trailing-edge flap of the model was significantly higher than the momentum required for controlling leading-edge flow separation and higher than the momentum required for controlling flow separation on the NACA 0015 at flight Reynolds numbers. The BART data 2 also indicated that combining multiple excitations would increase control authority.…”
Section: Trailing-edge Flap Actuatorsmentioning
confidence: 99%
See 1 more Smart Citation
“…The low Reynolds number SHL results on the BART model 2,3 indicated that the momentum required to control flow separation on the trailing-edge flap of the model was significantly higher than the momentum required for controlling leading-edge flow separation and higher than the momentum required for controlling flow separation on the NACA 0015 at flight Reynolds numbers. The BART data 2 also indicated that combining multiple excitations would increase control authority.…”
Section: Trailing-edge Flap Actuatorsmentioning
confidence: 99%
“…Low Reynolds number results of Melton et al 1,2,3 showed that periodic excitation was effective at controlling leading-edge flap shoulder separation, increasing the maximum lift coefficient, C L,max , by 10-15% at low (less than 5…”
mentioning
confidence: 99%
“…Numerous experimental [1,2,3,4,5,6,7,8,9,10,11,12] and numerical [13,14,15,16,17] studies were conducted in this area. Numerical methods using Computational Fluid Dynamics (CFD) techniques were widely used for simulating and evaluating the synthetic jets as active low method in controlling the low separation over lifting surfaces.…”
Section: Introductionmentioning
confidence: 99%
“…In 2011, feed forward neural network deep learning uses convolutional layers and pooling layers with a pure classi ication layer. The training process also eliminated the need to introduce unsupervised pre-training [8,9,10,11,12]. This method won various types of pattern recognition contests in 2011 [13], including the 2011 traf ic mark recognition contest [14] and other games.…”
Section: Introductionmentioning
confidence: 99%
“…The passenger car equivalent formula has different values in different places because each city's speed limit and traf ic composition is different. The passenger car equivalent presents different qualities under different circumstances [1,2].…”
Section: Introductionmentioning
confidence: 99%