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Issue 10 , December 2015

Plasmas for Aeronautics

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The 10th issue of Aerospace Lab is devoted to plasmas for aeronautics. The use of plasmas for aerodynamics and combustion has gained growing interest in the past 20 years, and a whole scientific community is now dedicated to this field of research. The content of this special issue reflects the diversity of the applications and of the physical conditions where plasmas are applied: from the subsonic to the supersonic regime, from combustion chambers to external aerodynamics, and from thermal plasmas to cold plasmas. Both experimental and modeling aspects are covered, as the complexity of the physics involved render the joint approach necessary. This issue will give the reader an overview of the current activities in this new field of research, and a glimpse of the numerous studies and applications of plasmas that are to come in aeronautics.

CONTENTS

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Plasmas for Aeronautics

Denis Packan (ONERA)

Plasma Aerodynamics: Current Status and Future Directions

J. Poggie (US Air Force Research Laboratory)
T. McLaughlin (US Air Force Academy)
S. Leonov (The Ohio State University)

A Short Review of Microwave and Laser Discharges for Supersonic Flow Control

D. Knight (Rutgers, The State University of New Jersey)

Numerical Simulations on the Effect and Efficiency of Long Linear Energy Deposition Ahead of a Supersonic Blunt Body: Toward a Laser Spike

P.-Q. Elias (ONERA)

Plasmas for High Speed Flow Control

R. Joussot, S. Coumar, V. Lago (ICARE, CNRS, Orléans)

Numerical Modeling of Dielectric Barrier Discharge Based Plasma Actuators for Flow Control: the COPAIER/CEDRE Example

G. Dufour, F. Rogier (ONERA)

Applications of Dielectric Barrier Discharges and Plasma Synthetic Jet Actuators at ONERA

F. Chedevergne, G. Casalis, O. Léon, M. Forte, F. Laurendeau, N. Szulga, O. Vermeersch, E. Piot (ONERA)

Mechanisms of Ethylene Flame Propagation Enhancement by O₂(a¹Δg)

T. Ombrello (U.S. Air Force Research Laboratory)
N. Popov (Moscow State University)

Experiments on Plasma-Assisted Combustion in a Supersonic Flow: Optimization of Plasma Position in Relation to the Fuel Injector

K.V. Savelkin, D.A. Yarantsev (Russian Academy of Sciences)
S.B. Leonov (Russian Academy of Sciences) (University of Notre Dame)

Ignition of Lean Air / Hydrocarbon Mixtures at Low Temperature by a Single Corona Discharge Nanosecond Pulse

S. Bentaleb, N. Blin-Simiand, P. Jeanney, L. Magne, N. Moreau, S. Pasquiers, P. Tardiveau (Université Paris-Sud and CNRS Université Paris-Saclay)

Aerospace Lab is an electronic journal dedicated to scientific progress in aeronautics and space research. Its featured technical fields therefore include aerodynamics, propulsion, materials, structures, physics, sensors, information processing, and system engineering.

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Previous issues

  • Aeroelasticity and Structural Dynamics
  • Design and Validation of Aerospace Control Systems: New Methods & Tools with Illustrations
  • Testing in Aerospace Research
  • Challenges in combustion for Aerospace Propulsion
  • Plasmas for Aeronautics
  • Life Prediction Methodologies for Materials and Structures
  • Aerial Robotics
  • Aeroacoustics
  • Flow Control: the Renewal of Aerodynamics?
  • Lightning Hazards to Aircraft and Launchers
  • Mastering Complexity
  • High Temperature Materials
  • CFD Platforms and Coupling
  • Optical Diagnostics of Flows
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