Optimal control of shock wave turbulent boundary layer interactions using micro-array actuation

Collection of Technical Papers - 3rd AIAA Flow Control Conference

Volumn 2, Issue , 2006, Pages 880-893

  Anderson, Bernhard H ^a   Tinapple, Jon ^b,d   Surber, Lewis ^c  

^a NASA GLENN RESEARCH CENTER   (United States)

^b WRIGHT PATTERSON AIR FORCE BASE   (United States)

^c UNIVERSAL TECHNOLOGY CORPORATION   (United States)

^d AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER THICKNESS; MICROARRAY FLOW CONTROL; RESPONSE SURFACE METHODOLOGY (RSM); SHOCK WAVE BOUNDARY LAYER (SWBL);

ACTUATORS; FLOW CONTROL; OPTIMAL CONTROL SYSTEMS; SHOCK WAVES; SUPERSONIC FLOW; TURBULENT FLOW;

BOUNDARY LAYERS;

EID: 33845270159     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Tjonneland, E., "The Design, Development, and Testing of a Supersonic Transport Intake System," AGARD-CP-91-71, paper presented at the 38th meeting of the AGARD Propulsion and Energetics Panel, Sandefjord, Norway, September 1971.
2. Fukuda, M. K, Hingst, W. G., and Reshotko, E., "Control of Shock Wave-Boundary Layer Interactions by Bleed in Supersonic Mixed Compression Inlets," NASA CR-2595, August, 1975
3. Syberg, J. and Konsek, J. L., "Bleed system design technology for supersonic inlets", Jour. of Aircraft, Vol. 10, No. 7.
4. Box, G. E. P., Hunter, W. G., and Hunter, J. S., "Statistics for Experimenters," John Wiley, New York
5. NPARC Alliance, "The Wind-US Code", http://www/grc.nasa/www/ Wind-US docs [cited 13 June 2004.
6. Bush, R. H., Power, G. D., and Towne, C. E., "Wind-US: The Production Flow Solver of the NPRAC Alliance", AIAA-1998-0935, Januar7y 1998.
7. Anderson, B. H., Tinapple, J., and Surber, L., "Optimal Micro-Array Actuation Control for Shock Wave Boundary Layer Interactions in Supersonic Inlets", Proposed NASA TM, 2006.