A Robust Design Methodology for Optimal Micro-Scale Secondary Flow Control in Compact Inlet Diffusers.

A Robust Design Methodology for Optimal Micro-Scale Secondary Flow Control in Compact Inlet Diffusers.

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2002

Pub. Year:

2002

No.:

2002-0541

Paper no.:

2002-0541

Pages:

12

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001706
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	40th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2002.01.14-2002.01.17
Note for article:	40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 14-17 January 2002

Similar Items:

1 Technical Paper Design-of-Experiments to Reduce Life-Cycle Costs in Combat Aircraft Inlets. Anderson, B.H., Baust, H.D., Agrell, J. American Institute of Aeronautics and Astronautics	7 Technical Paper Experimental Investigation of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser N. Harrison, J. Anderson, J. Fleming, W. Ng American Institute of Aeronautics and Astronautics
2 Technical Paper A Non-Intrusive Sensing Technique to Infer Optimal Flow Control in Serpentine Inlets J. Anderson, W. Ng, R. Burdisso, P. Truax, D. Miller, M. Niestroy American Institute of Aeronautics and Astronautics	8 Technical Paper Practical design methodologies for robust nonlinear flight control Cheng, V.H.L., Njaka, C.E., Menon, P.K. American Institute of Aeronautics and Astronautics
3 Technical Paper An Approach for Robust Micro-Scale Materials Design Under Unparameterizable Variability Choi, H., Austin , R., Shepherd, J., Allen, J., McDowell, D., Mistree, F. American Institute of Aeronautics and Astronautics	9 Technical Paper A methodology for the robust cooling design of an HSCT combustor liner Mavris, D.N., Roth, B.A. American Institute of Aeronautics and Astronautics
4 Technical Paper Optimal Design of Passive Flow Control for a Boundary-Layer-Ingesting Offset Inlet Using Design-of-Experiments B. Allan, L. Owens, J. Lin American Institute of Aeronautics and Astronautics	10 Technical Paper Micro-Vortex Generator Flow Control for Supersonic Engine Inlets H. Babinsky, N. Makinson, C. Morgan American Institute of Aeronautics and Astronautics
5 Technical Paper THREE-DIMENSIONAL VISCOUS DESIGN METHODOLOGY FOR ADVANCED TECHNOLOGY AIRCRAFT SUPERSONIC INLET SYSYTEMS Anderson, Bernhard H. National Aeronautics and Space Administration	11 Technical Paper Optimal Design of Compact Sour Gear Reductions Savage,M., Lattime, S.B., Kimmel, J.A., Coe, H.H. National Aeronautics and Space Adminstration
6 Technical Paper Computer Analysis of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser N. Harrison, J. Anderson, J. Fleming American Institute of Aeronautics and Astronautics	12 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

1

2

3

4

5

6

7

8

9

10

11

12