6 Wind and Water Tunnel Equipment
435
Fig. 6.63 Nozzle diameter = 0.42 m arc wind tunnel (FD-04, Ma = 0.6−12, China
Academy of Aerospace Aerodynamics)
Fig. 6.64 Nozzle diameter = 1.0 m arc wind tunnel (FD-15, Ma = 0.6−10. It
can undertake all kinds of material ablation properties, particle erosion, cone body
heat layer induced ablation heat through waves’ roll moments, pneumatic optical
transmission, and re-entry physical phenomenon tests. China Academy of Aerospace
Aerodynamics.)
demand of basic test time”, and “testing full-size or close to full-scale model”.
The reproducibility of the ground test of hypersonic aircraft has been realized, and it provides an irreplaceable test method for the key technologies of
China’s major engineering projects and the basic research of high-temperature
aerodynamics.
435
Fig. 6.63 Nozzle diameter = 0.42 m arc wind tunnel (FD-04, Ma = 0.6−12, China
Academy of Aerospace Aerodynamics)
Fig. 6.64 Nozzle diameter = 1.0 m arc wind tunnel (FD-15, Ma = 0.6−10. It
can undertake all kinds of material ablation properties, particle erosion, cone body
heat layer induced ablation heat through waves’ roll moments, pneumatic optical
transmission, and re-entry physical phenomenon tests. China Academy of Aerospace
Aerodynamics.)
demand of basic test time”, and “testing full-size or close to full-scale model”.
The reproducibility of the ground test of hypersonic aircraft has been realized, and it provides an irreplaceable test method for the key technologies of
China’s major engineering projects and the basic research of high-temperature
aerodynamics.