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contributor authorKing, W. D.
contributor authorTurvey, D. E.
contributor authorWilliams, D.
contributor authorLlewellyn, D. J.
date accessioned2017-06-09T16:01:22Z
date available2017-06-09T16:01:22Z
date copyright1984/03/01
date issued1984
identifier issn0739-0572
identifier otherams-59.pdf
identifier urihttp://onlinelibrary.yabesh.ir/handle/yetl/4199510
description abstractMeasurements have been made of airflow velocities and cloud liquid water contents from selected positions around the fuselage of an F-27 aircraft. The airflow measurements away from the propeller inflow region are in reasonable agreement with those calculated in Part I. The liquid water measurements were made using two CSIRO hot-wire probes, one of which could be positioned at distances of 15?60 cm from the fuselage. Results of these comparisons showed that the enhancement factors calculated in Part I appear quite reasonable and that corrections can consequently be made to allow for sampling errors caused by fuselage-related flow distortions. The comparisons also show that there are additional sampling errors as large as 10% which depend on position of the probe relative to the wings and propeller. For the F-27 these additional effects decrease substantially with increasing aircraft speed.
publisherAmerican Meteorological Society
titleAir Flow and Particle Trajectories around Aircraft Fuselages. II: Measurements
typeJournal Paper
journal volume1
journal issue1
journal titleJournal of Atmospheric and Oceanic Technology
identifier doi10.1175/1520-0426(1984)001<0014:AFAPTA>2.0.CO;2
journal fristpage14
journal lastpage21
treeJournal of Atmospheric and Oceanic Technology:;1984:;volume( 001 ):;issue: 001
contenttypeFulltext


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