Accession Number ADA582265
Title Characterisation and Airborne Deployment of a New Counterflow Virtual Impactor Inlet.
Publication Date Jun 2012
Media Count 13p
Personal Author A. Sorooshian F. J. Brechtel S. Dey T. Shingler Z. Wang
Abstract A new counterflow virtual impactor (CVI) inlet is introduced with details of its design, laboratory characterisation tests and deployment on an aircraft during the 2011 Eastern Pacific Emitted Aerosol Cloud Experiment (EPEACE). The CVI inlet addresses three key issues in previous designs; in particular, the inlet operates with: (1) negligible organic contamination; (2) a significant sample flow rate to downstream instruments (approx. 15 1 min(-1)) that reduces the need for dilution; and (3) a high level of accessibility to the probe interior for cleaning. Wind tunnel experiments characterised the cut size of sampled droplets and the particle size-dependent transmission efficiency in various parts of the probe. For a range of counter-flow rates and air velocities, the measured cut size was between 8.7-13.1 microns. The mean percentage error between cut size measurements and predictions from aerodynamic drag theory is 1.7 %. The CVI was deployed on the Center for Interdisciplinary Remotely Piloted Aircraft Studies (CIRPAS) Twin Otter for thirty flights during E-PEACE to study aerosol-cloud-radiation interactions off the central coast of California in July and August 2011. Results are reported to assess the performance of the inlet including comparisons of particle number concentration downstream of the CVI and cloud drop number concentration measured by two independent aircraft probes. Measurements downstream of the CVI are also examined from one representative case flight coordinated with shipboard-emitted smoke that was intercepted in cloud by the Twin Otter.
Keywords Airborne
Cirpas(Center for interdisciplinary remotely piloted aircraf
Cvi(Counterflow virtual impactor)
Deployment
Epeace(Eastern pacific emitted aerosol cloud experiment)
Inlets
Mfc(Mass flow controller)
Velocity
Wind tunnel tests


 
Source Agency Non Paid ADAS
NTIS Subject Category 51B - Aeronautics
74G - Military Operations, Strategy, & Tactics
Corporate Author California Inst. of Tech., Pasadena. Dept. of Environmental Engineering Science.
Document Type Journal article
Title Note Journal article.
NTIS Issue Number 1326
Contract Number N00014-10-1-0783 N00014-10-1-0811

Science and Technology Highlights

See a sampling of the latest scientific, technical and engineering information from NTIS in the NTIS Technical Reports Newsletter

Acrobat Reader Mobile    Acrobat Reader