BODY DRAG, FEATHER DRAG AND INTERFERENCE DRAG OF THE MOUNTING STRUT IN A PEREGRINE FALCON

falcon body and a smooth-surfaced model of the body were 0.24 and 0.14, respectively, at air speeds between 10.0 and 14.5 ms"1. These values were measured with a drag balance in a wind tunnel, and use the maximum cross-sectional area of the body as a reference area. The difference between the v...

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Main Authors: Falco Peregrinus, A. Tucker
Other Authors: The Pennsylvania State University CiteSeerX Archives
Format: Text
Language:English
Published: 1989
Subjects:
Online Access:http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.622.4480
http://jeb.biologists.org/content/149/1/449.full.pdf
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spelling ftciteseerx:oai:CiteSeerX.psu:10.1.1.622.4480 2023-05-15T17:55:13+02:00 BODY DRAG, FEATHER DRAG AND INTERFERENCE DRAG OF THE MOUNTING STRUT IN A PEREGRINE FALCON Falco Peregrinus A. Tucker The Pennsylvania State University CiteSeerX Archives 1989 application/pdf http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.622.4480 http://jeb.biologists.org/content/149/1/449.full.pdf en eng http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.622.4480 http://jeb.biologists.org/content/149/1/449.full.pdf Metadata may be used without restrictions as long as the oai identifier remains attached to it. http://jeb.biologists.org/content/149/1/449.full.pdf text 1989 ftciteseerx 2016-01-08T15:04:12Z falcon body and a smooth-surfaced model of the body were 0.24 and 0.14, respectively, at air speeds between 10.0 and 14.5 ms"1. These values were measured with a drag balance in a wind tunnel, and use the maximum cross-sectional area of the body as a reference area. The difference between the values indicates the effect of the feathers on body drag. Both values for CD.B a r e lower than those predicted from most other studies of avian body drag, which yield estimates of CQ.B up to 0.41. 2. Several factors must be controlled to measure minimum drag on a frozen body. These include the condition of the feathers, the angle of the head and tail relative to the direction of air flow, and the interference drag generated by the drag balance and the strut on which the body is mounted. 3. This study describes techniques for measuring the interference drag gener-ated by (a) the drag balance and mounting strut together and (b) the mounting strut alone. Corrections for interference drag may reduce the apparent body drag by more than 20 %. 4. A gliding Harris ' hawk (Parabuteo unicinctus), which has a body similar to that of the falcon in size and proportions, has an estimated body drag coefficient of 0.18. This value can be used to compute the profile drag coefficients of Harris' hawk wings when combined with data for this species in the adjoining paper (Tucker and Heine, 1990). Text peregrine falcon Unknown Heine ENVELOPE(167.450,167.450,-78.083,-78.083)
institution Open Polar
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description falcon body and a smooth-surfaced model of the body were 0.24 and 0.14, respectively, at air speeds between 10.0 and 14.5 ms"1. These values were measured with a drag balance in a wind tunnel, and use the maximum cross-sectional area of the body as a reference area. The difference between the values indicates the effect of the feathers on body drag. Both values for CD.B a r e lower than those predicted from most other studies of avian body drag, which yield estimates of CQ.B up to 0.41. 2. Several factors must be controlled to measure minimum drag on a frozen body. These include the condition of the feathers, the angle of the head and tail relative to the direction of air flow, and the interference drag generated by the drag balance and the strut on which the body is mounted. 3. This study describes techniques for measuring the interference drag gener-ated by (a) the drag balance and mounting strut together and (b) the mounting strut alone. Corrections for interference drag may reduce the apparent body drag by more than 20 %. 4. A gliding Harris ' hawk (Parabuteo unicinctus), which has a body similar to that of the falcon in size and proportions, has an estimated body drag coefficient of 0.18. This value can be used to compute the profile drag coefficients of Harris' hawk wings when combined with data for this species in the adjoining paper (Tucker and Heine, 1990).
author2 The Pennsylvania State University CiteSeerX Archives
format Text
author Falco Peregrinus
A. Tucker
spellingShingle Falco Peregrinus
A. Tucker
BODY DRAG, FEATHER DRAG AND INTERFERENCE DRAG OF THE MOUNTING STRUT IN A PEREGRINE FALCON
author_facet Falco Peregrinus
A. Tucker
author_sort Falco Peregrinus
title BODY DRAG, FEATHER DRAG AND INTERFERENCE DRAG OF THE MOUNTING STRUT IN A PEREGRINE FALCON
title_short BODY DRAG, FEATHER DRAG AND INTERFERENCE DRAG OF THE MOUNTING STRUT IN A PEREGRINE FALCON
title_full BODY DRAG, FEATHER DRAG AND INTERFERENCE DRAG OF THE MOUNTING STRUT IN A PEREGRINE FALCON
title_fullStr BODY DRAG, FEATHER DRAG AND INTERFERENCE DRAG OF THE MOUNTING STRUT IN A PEREGRINE FALCON
title_full_unstemmed BODY DRAG, FEATHER DRAG AND INTERFERENCE DRAG OF THE MOUNTING STRUT IN A PEREGRINE FALCON
title_sort body drag, feather drag and interference drag of the mounting strut in a peregrine falcon
publishDate 1989
url http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.622.4480
http://jeb.biologists.org/content/149/1/449.full.pdf
long_lat ENVELOPE(167.450,167.450,-78.083,-78.083)
geographic Heine
geographic_facet Heine
genre peregrine falcon
genre_facet peregrine falcon
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http://jeb.biologists.org/content/149/1/449.full.pdf
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