Drag Reduction by Laser-Plasma Energy Addition in Hypersonic Flow
- Instituto Nacional de Pesquisas Espaciais, 12630-000 Cachoeira Paulista (Brazil)
- Instituto de Estudos Avancados, 12228-001 Sao Jose dos Campos (Brazil)
- Rensselaer Polytechnic Institute, Troy, New York 12180-3590 (United States)
An experimental study was conducted to investigate the drag reduction by laser-plasma energy addition in a low density Mach 7 hypersonic flow. The experiments were conducted in a shock tunnel and the optical beam of a high power pulsed CO{sub 2} TEA laser operating with 7 J of energy and 30 MW peak power was focused to generate the plasma upstream of a hemispherical model installed in the tunnel test section. The non-intrusive schlieren optical technique was used to visualize the effects of the energy addition to hypersonic flow, from the plasma generation until the mitigation of the shock wave profile over the model surface. Aside the optical technique, a piezoelectric pressure transducer was used to measure the impact pressure at stagnation point of the hemispherical model and the pressure reduction could be observed.
- OSTI ID:
- 21137118
- Journal Information:
- AIP Conference Proceedings, Vol. 997, Issue 1; Conference: 5. international symposium on beamed energy propulsion, Kailua-Kona, HI (United States), 12-15 Nov 2007; Other Information: DOI: 10.1063/1.2931907; (c) 2008 American Institute of Physics; Country of input: International Atomic Energy Agency (IAEA); ISSN 0094-243X
- Country of Publication:
- United States
- Language:
- English
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