A new aircraft inlet for sampling interstitial aerosol: Design methodology, modeling, and wind tunnel tests

Aerosol Science and Technology

Volumn 47, Issue 8, 2013, Pages 885-894

  Moharreri, Arash ^a   Craig, Lucas ^a   Rogers, David C ^b   Dhaniyala, Suresh ^a  

^a CLARKSON UNIVERSITY   (United States)

^b NATIONAL CENTER FOR ATMOSPHERIC RESEARCH   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS SIMULATIONS; DESIGN METHODOLOGY; FLOW REQUIREMENTS; INTERSTITIAL PARTICLES; PERFORMANCE CHARACTERIZATION; PROTOTYPE MODELS; TEST METHODOLOGY; WIND TUNNEL TESTS;

AEROSOLS; BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; DESIGN; DROPS; EXPERIMENTS; HOUSING; INTAKE SYSTEMS; WIND STRESS;

AIRCRAFT;

AEROSOL; AIRCRAFT; ARTICLE; ARTIFACT; BODY BUILD; BOUNDARY LAYER; COMPUTATIONAL FLUID DYNAMICS; FLOW RATE; PRIORITY JOURNAL; SAMPLER; SIMULATION;

EID: 84879089909     PISSN: 02786826     EISSN: 15217388     Source Type: Journal    
DOI: 10.1080/02786826.2013.800186     Document Type: Article

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