Microactuator Arrays for Sublayer Control in Turbulent Boundary Layers Using the Electrokinetic Principle

Microactuator Arrays for Sublayer Control in Turbulent Boundary Layers Using the Electrokinetic Principle

Author(s):

Diez-Garias, Francisco J. ( Laboratory for Turbulence & Combustion (LTC) Department of Aerospace Engineering The University of Michigan )
Dahm, Werner J.A.
Paul, Phillip H.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-0548

Paper no.:

00-0548

Page(from):

1

Page(to):

18

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050874
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospaces Science Meeting and Exhibit
Conf. info. (Number):	38th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2000.01.10-2000.01.13
Note for article:	38th Aerospace Sciences Meeting & Exhibit 10-13 January 2000 / Reno, NV

Similar Items:

1 Technical Paper Micro Electro Kinetic Actuator (MEKA) Arrays for Active Sublayer Control of Turbulent Boundary Layers Diez, F.J., Dahm, W.J.A. American Institute of Aeronautics and Astronautics	7 Technical Paper Compressibility Effects on Entrainment and Mixing in Supersonic Planar Turbulent Wakes Nakagawa, Masaki, Dahm, Werner J.A. American Institute of Aeronautics and Astronautics
2 Technical Paper Model for the control of sound radiation from an aircraft panel excited by a turbulent boundary layer using impedance control Curtis, Alan R.D., Remington, Paul J. American Institute of Aeronautics and Astronautics	8 Technical Paper Mach Number Effects on Entrainment and Mixing in Supersonic Planar Turbulent Wakes Nakagawa, Masaki, Dahm, Werner J.A. American Institute of Aeronautics and Astronautics
3 Technical Paper Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro-Array Actuation B. Anderson, J. Tinapple, L. Surber American Institute of Aeronautics and Astronautics	9 Technical Paper Velocity Measurements in the Near-Field of Supersonic Planar Turbulent Wakes Nakagawa, Masaki, Dahm, Werner J.A. American Institute of Aeronautics and Astronautics
4 Technical Paper Control of Normal Shock Wave/ Turbulent Boundary Layer Interactions Using Streamwise Grooves. Smith, A.N., Holden, H.A., Babinsky, H., Fulker, J.L., Ashill, P.R. American Institute of Aeronautics and Astronautics	10 Technical Paper Control of shock wave/turbulent boundary layer interactions using tangential injection Donovan, J.F. American Institute of Aeronautics and Astronautics
5 Technical Paper Control of Normal Shock Wave/Turbulent Boundary-Layer Interaction Using Streamwise Slots Smith,A.N., Babinsky,H., Fulker,J.L., Ashill,P.A. American Institute of Aeronautics and Astronautics	11 Technical Paper Control of Turbulent Boundary-Layer Separation using Micro-Vortex Generators Lin, J. C. American Institute of Aeronautics and Astronautics
6 Technical Paper Compressibility effects on entrainment and mixing in supersonic planar turbulent wakes Nakagawa, Masaki, Dahm, Werner J.A. American Institute of Aeronautics and Astronautics	12 Technical Paper Control of turbulent boundary-layer separation using micro-vortex generators Lin, J.C. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12