A new friction factor model and entrance loss coefficient for honeycomb annular gas seals

A new experimental friction factor model for a honeycomb surface was develo ped using a static seal tester. Three clearances and three lengths were tes ted for the seals, and Reynolds number ranged from 3000 to 49,000. It was f ound that the friction factor was a function of Reynolds number and seal cl earance only. The clearance effect was dominant and the friction factor was found to increase with increased clearance. A new uncertainty analysis was developed for the experimental friction factor when calculating friction f actor using Mach number curve fit. The entrance loss coefficient was found to be constant for both smooth and honeycomb seals. The entrance loss coeff icient of Honeycomb seals was found to be 50 percent higher than that of sm ooth seals. [S0742-4787(00)02102-0].