Numerical Investigation of Pulsed Thermal Pertubration in Supersonic Boundary Layer

Numerical Investigation of Pulsed Thermal Pertubration in Supersonic Boundary Layer

Author(s):

H. Yan ( Wright State University, Dayton, OH )
D. Gaitonde ( U.S. Air Force Research Laboratory, Dayton, OH )
J. Shang ( Wright State University, Dayton, OH )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Plasmadynamics and Lasers Conference

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-3887

Paper no.:

AIAA Paper 2007-3887

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200715 [CD-ROM 2007 Disc 15]

Type:

Technical Paper

Details

TDL ID:	ZA00049506
Series ID:	PA00000148
Conf. info. (Name):	AIAA Plasmadynamics and Lasers Conference ; International Conference on MHD Energy Conversion
Conf. info. (Number):	38th ; 16th
Conf. info. (Venue):	Miami, Florida
Conf. info. (Date):	2007.06.25-2007.06.28
Note for article:	38th AIAA Plasmadynamics and Lasers Conference in conjunction with the 16th International Conference on MHD Energy Conversion , Miami, Florida, June 25-28, 2007

Similar Items:

1 Technical Paper Investigation of Localized Arc Filament Plasma Actuator in Supersonic Boundary Layer H. Yan, D. Gaitonde, J. Shang American Institute of Aeronautics and Astronautics	7 Technical Paper Numerical simulation of supersonic turbulent boundary layer flow with mild pressure gradient Fick, E.T., Buter, T.A., Gaitonde, D. American Institute of Aeronautics and Astronautics
2 Technical Paper Supersonic Flow Control by Pulsed Thermal Bump H. Yan, D. Gaitonde, J. Shang American Institute of Aeronautics and Astronautics	8 Technical Paper Hypersonic Flow Control Utilizing Electromagnetic-Aerodynamic Interaction J. Shang, P. Huang,, H. Yan, S. Surzhikov, D. Gaitonde American Institute of Aeronautics and Astronautics
3 Technical Paper The Effect of a Thermal Bump in Supersonic Flow H. Yan, D. Gaitonde, J. Shang American Institute of Aeronautics and Astronautics	9 Technical Paper Control of Edney IV Interaction by Energy Pulse H. Yan, D. Gaitonde American Institute of Aeronautics and Astronautics
4 Technical Paper Numerical Study on Effect of a Thermal Bump in Supersonic Flow Control H. Yan, D. Gaitonde American Institute of Aeronautics and Astronautics	10 Technical Paper Effect of Energy Pulse on Edney IV Interaction H. Yan, D. Gaitonde American Institute of Aeronautics and Astronautics
5 Technical Paper Numerical Investigation of New Topologies in Strong Crossing Shock-Wave/Turbulent Boundary Layer Interactions Schmisseur, J. D., Gaitonde, Datta V. American Institute of Aeronautics and Astronautics	11 Technical Paper Stability of thermally -induced perturbation in compressible flow Yan, H., Gaitonde, D. American Institute of Aeronautics and Astronautics
6 Technical Paper On 3-D shock wave/turbulent boundary layer interactions at Mach 4 Gaitonde, D., Shang, J.S. American Institute of Aeronautics and Astronautics	12 Technical Paper Effect of Thermally-Induced Surface Perturbation in Compressible Flow H. Yan, D. Gaitonde American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12