Hologram showing transonic air flow over NACA 0012 aerofoil in a wind tunnel

Hologram showing transonic air flow over NACA 0012 aerofoil in a wind tunnel at a free stream Mach No. of 0.93, taken at Cranfield Institute of Technology

Details

Category:
Optics
Object Number:
1992-1110
Measurements:
overall: 3kg
type:
hologram
credit:
British Aerospace plc