• 1089 Citations
  • 15 h-Index
20042019
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Fingerprint Dive into the research topics where Jesse C Little is active. These topic labels come from the works of this person. Together they form a unique fingerprint.

  • 3 Similar Profiles
Airfoils Engineering & Materials Science
Actuators Engineering & Materials Science
Plasmas Engineering & Materials Science
Flow control Engineering & Materials Science
Boundary layers Engineering & Materials Science
Feedback control Engineering & Materials Science
cavity flow Physics & Astronomy
Mach number Engineering & Materials Science

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Research Output 2004 2019

  • 1089 Citations
  • 15 h-Index
  • 54 Conference contribution
  • 17 Article

Comparison of various fluidic oscillators for separation control on a wall-mounted hump

Otto, C., Tewes, P., Little, J. C. & Woszidlo, R., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fluidics
Flow control
Geometry
Flow visualization
Pressure measurement

Experimental study of swept impinging oblique shock boundary layer interaction

Padmanabhan, S., Maldonado, J. C., Threadgill, J. A. S. & Little, J. C., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Boundary layers
Pressure measurement
Velocity measurement
Pressure transducers
Flow visualization

Post-stall flow control using nanosecond pulse driven dielectric barrier discharge plasma actuators

Little, J. C., Singh, A., Ashcraft, T. & Durasiewicz, C., Jan 10 2019, In : Plasma Sources Science and Technology. 28, 1, 014002.

Research output: Contribution to journalArticle

plasma jets
actuators
pulses
bluff bodies
static pressure

Transitional shock wave boundary layer interactions on a compression ramp at mach 4

Threadgill, J. A. S., Little, J. C. & Wernz, S. H., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shock waves
Mach number
Boundary layers
Reynolds number
Wind tunnels
5 Citations (Scopus)

A comparative flow physics study of Ns-DBD vs Ac-DBD plasma actuators for transient separation control on a NACA 0012 airfoil

Durasiewicz, C., Singh, A. & Little, J. C., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airfoils
Actuators
Physics
Plasmas
Time delay