An evaluation of the community aerosol inlet for the NCAR C-130 research aircraft

Based on both in-flight measurements and a fluid dynamics model, airflow in the National Center for Atmospheric Research (NCAR) Community Aerosol Inle t (CAI) is similar to fully developed pipe flow. Distortions of the velocit y field were pronounced when suction to inlet tubes was shut off, but condi tions were otherwise insensitive to all flight parameters but airspeed. The principal value of the multiuser CAI system for NCAR's C-130 is that it de celerates air with no curves until the velocity has been reduced to 10 m s( -1). It then supplies uniformly modified air (after turbulent losses) to al l users, enabling valid closure experiments. Chemical data from both the First Aerosol Characterization Experiment (ACE- 1) and the Second Community Aerosol Inlet Evaluation Program (CAINE-II) cle arly indicate that while passing efficiency for submicron aerosol is accept able, very little of the sea salt mode mass is transmitted by the CAI to in struments inside the aircraft. Comparisons between chemical samples from an external total aerosol sampler and samplers behind the CAI indicate that 7 0%-90% of the sea salt mass is unable to pass the CAI. The 50% cut size is about 3 mum, but the precise details of the efficiency curve are obscured b y the difficulty of measuring a reference ambient aerosol distribution. The loss of particle mass becomes very significant above 3 mum, but the size c ut is not sharp. These conclusions are supported by calculated particle tra nsmission efficiencies for the CAI.