Photoacoustic hygrometer for icing wind tunnel water content measurement: design, analysis, and intercomparison

نویسندگان

چکیده

Abstract. This work describes the latest design, calibration and application of a near-infrared laser diode-based photoacoustic (PA) hygrometer developed for total water content measurement in simulated atmospheric freezing precipitation high ice conditions with relevance fundamental icing research, aviation testing, certification. The single-wavelength single-pass PA absorption cell is calibrated molar vapor fractions two-pressure humidity generator integrated into instrument. Laboratory showed an estimated accuracy better than 3.3 % mole fraction range 510–12 360 ppm (5 from 250–21 200 ppm) theoretical limit detection (3σ) 3.2 ppm. examined combination basic isokinetic evaporator probe (IKP) sampling system designed wind tunnel applications, which general description condensed (CWC) measurements uncertainties are presented. Despite current limitation IKP to hydrometeor mass flux below 90 gm-2s-1, CWC 20 achieved by instrument above 0.14 g m−3 cold air (−30 ∘C) suitable background measurement. Results comparison Cranfield University drizzle rain show agreement two instruments within %, demonstrates potential hygrometers conditions.

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

A two-channel, tunable diode laser-based hygrometer for measurement of water vapor and cirrus cloud ice water content in the upper troposphere and lower stratosphere

The recently developed NOAA Water instrument is a two-channel, closed-path, tunable diode laser absorption spectrometer designed for the measurement of upper troposphere/lower stratosphere water vapor and enhanced total water (vapor + inertially enhanced condensed phase) from the NASA Global Hawk unmanned aircraft system (UAS) or other high-altitude research aircraft. The instrument utilizes wa...

متن کامل

design, analysis and optimization of the ejector injection nozzle supersonic wind tunnel

in this article, an algorithm for designing of a supersonic wind tunnel injection nozzle ejector is presented and based on this algorithm, a new ejector is designed for a supersonic wind tunnel. the injection nozzle consists of a volute, a nozzle, and several vanes. designed injection nozzle is simulated numerically, and the results are compared with the present injection nozzle. the results sh...

متن کامل

On-road and wind-tunnel measurement of motorcycle helmet noise.

The noise source mechanisms involved in motorcycling include various aerodynamic sources and engine noise. The problem of noise source identification requires extensive data acquisition of a type and level that have not previously been applied. Data acquisition on track and on road are problematic due to rider safety constraints and the portability of appropriate instrumentation. One way to add...

متن کامل

Aerodynamic Analysis and Wind Tunnel Test for Flapping-wing Mavs

A lightweight flapping-wing micro air vehicle (MAV) was designed and built and successfully filed in the sky. The unsteady aerodynamics associated with this MAV was detailedly studied by using the method of computational fluid dynamics (CFD).The variations of different parameters of the flapping MAV, such as flapping amplitude, pitch amplitude and flapping frequency, were investigated with nume...

متن کامل

Wind Turbine Performance Under Icing Conditions

Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, 306 Talbot Laboratory, 104 S. Wright Street Urbana. IL 61801-2935 The effects of rime ice on horizontal axis wind turbine performance were estimated. For typzcal supercooled fog conditions found in cold northern regions, four rime ice accretwns on the 5809 wmd turbine airfoil were predicted usi...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Atmospheric Measurement Techniques

سال: 2021

ISSN: ['1867-1381', '1867-8548']

DOI: https://doi.org/10.5194/amt-14-2477-2021