Power consumption, discharge capacitance and light emission as measures for thrust production of dielectric barrier discharge plasma actuators

By J. Kriegseis, Sven Grundmann, Cameron Tropea. 2011

145 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Electrical and Electronic Engineering, Radiology, Nuclear Medicine and Imaging

View Paper: https://www.semanticscholar.org/paper/bd47994e0cc12e67043bdd67e0dbbed2997a0fd5

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Marios Kotsonis
2. N. Benard
3. Eric Moreau
4. Igor V. Adamovich

In Electrical and Electronic Engineering

1. Marios Kotsonis
2. N. Benard
3. X. Tu
4. Eric Moreau
5. G. Pietsch
6. V. Gibalov
7. J. Whitehead
8. Igor V. Adamovich

In Radiology, Nuclear Medicine and Imaging

1. Marios Kotsonis
2. X. Tu
3. N. Benard
4. Eric Moreau
5. G. Pietsch
6. V. Gibalov
7. J. Whitehead
8. R. Brandenburg

Citations in the corpus

• Diagnostics for characterisation of plasma actuators (2015, background): “Wilke [132] and later Kriegseis et al [88] and Neumann et al [87] assumed that the pressure gradient is significantly smaller than the body force and neglected it altogether.”
• Dry reforming of methane over a Ni/Al2O3 catalyst in a coaxial dielectric barrier discharge reactor (2011, methodology): “This shape has been observed previously with packed bed DBD with a BaTiO3 packing [21], as well as plasma actuators [32].”
• Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, methodology): “A more recent study (Kriegseis et al. 2011b) confirms that the thrust increases nearly linearly with the consumed power (Fig.”