A.C. plasma anemometer for hypersonic mach number experiments

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 3671-3685

  Matlis, Eric H ^a,c,d   Corke, Thomas C ^a,d   Gogineni, Sivaram P ^b,d  

^a UNIVERSITY OF NOTRE DAME   (United States)

^b INNOVATIVE SCIENTIFIC SOLUTIONS INC   (United States)

^c AME Dept   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; ELECTRODES; FREQUENCY RESPONSE; GAS TURBINES; HYPERSONIC FLOW; HYSTERESIS; NUMBER THEORY; TEMPERATURE DISTRIBUTION;

MACH NUMBER; PLASMA ANEMOMETER; PLASMA DISCHARGES;

PLASMA APPLICATIONS;

EID: 30744477998     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-952     Document Type: Conference Paper

References (10)

1. Matlis, E. and Corke, T., "Quantitative Hot-Wire Measurements in Supersonic Boundary Layers." FEDSM'03,ASME/JSME Joint Fluids Engineering Conference., ASME, July 2003.
2. Morkovin, M., "Fluctuations and Hot-Wire Anemometry in Compressible Flows." AGARDograph 24, 1956.
3. Sheplak, M., Spina, E., and McGinley, C., "Progress in Hot-Film Anemometry for Hypersonic Flow," Experimental Thermal and Fluid Science, Vol. 13, No. 1, 1996, pp. 21-28.
4. Lindvall, F., "A Glow Discharge Anemometer," AIEE Trans., 1934, f53.
5. Fucks, W., "Untersunchung der Betreibeeigenschaften des Vorstromanemometers," NACA TN-1178, 1944, Translated 1947.
6. Mettler, R., The Anemometric Application of an Electrical Glow Discharge in Transverse Air Streams, Ph.D. thesis, California Institute of Technology, 1949.
7. Werner, F. D., The Corona Anemometer and its Application to Study of the Effect of Stilling Chamber Turbulence on Test Section Turbulence in a Wind Tunnel at Mach Number Three., Ph.D. thesis, University of Minnesota, 1955.
8. Vrebalovich, T., The Development of Direct- and Alternating-Current Glow-Discharge Anemometers for the Study of Turbulence Phenomena in Supersonic Flow., Ph.D. thesis, California Institute of Technology, 1954, JPL Report 20-81.
9. Post, M. and Corke, T., "Separation Control on High Angle of Attack Airfoil using Plasma Actuators," AIAA Paper 2003-1024, 2003, accepted AIAA J.
10. Enloe, L., McLauglin, T., CanDyken, R., Kachner, K., Jumper, E., and Corke, T., "Mechanisms and Response of a Single Dielectric Barrier Plasma Actuator," AIAA Paper 2003-1021, 2003.