Budget Amount *help |
¥4,680,000 (Direct Cost: ¥3,600,000、Indirect Cost: ¥1,080,000)
Fiscal Year 2010: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2009: ¥1,170,000 (Direct Cost: ¥900,000、Indirect Cost: ¥270,000)
Fiscal Year 2008: ¥2,600,000 (Direct Cost: ¥2,000,000、Indirect Cost: ¥600,000)
|
Research Abstract |
A normal shock wave in a constant area duct such as an isolator in a scram jet engine interacts with a wall boundary layer to form a pseudo-shock wave. Effects of the upstream boundary layer on a pseudo-shock wave are experimentally and theoretically clarified. Also, an optical system for measuring a complex shock containing supersonic flow quantitatively is presented. Further, compressible flow in curved ducts is experimentally studied.
|