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

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

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