2004
DOI: 10.1017/s0001924000000282
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Design methodology and performance of an indraft wind tunnel

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Cited by 55 publications
(54 citation statements)
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References 12 publications
(22 reference statements)
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“…The relative contributions to drag coefficient, Figure 14, show a far more consistent fore-body drag contribution with a reducing base drag with increasing top angle up to 16 o . On the side slant, the surface pressures show fully attached flow for 4 o and 8 o , at angles greater than 8 o there is a suction peak on the leading edge of the slant followed by pressure recovery over the slant length indicating reattachment.…”
Section: A -Model Frontal Area Da -Area Of Influence Of Each Tapping mentioning
confidence: 86%
See 1 more Smart Citation
“…The relative contributions to drag coefficient, Figure 14, show a far more consistent fore-body drag contribution with a reducing base drag with increasing top angle up to 16 o . On the side slant, the surface pressures show fully attached flow for 4 o and 8 o , at angles greater than 8 o there is a suction peak on the leading edge of the slant followed by pressure recovery over the slant length indicating reattachment.…”
Section: A -Model Frontal Area Da -Area Of Influence Of Each Tapping mentioning
confidence: 86%
“…All testing was carried out in the Loughborough University Wind Tunnel, full details of which can be found in Johl, Passmore & Render [16].…”
Section: The Facilitiesmentioning
confidence: 99%
“…Testing was performed in the Loughborough University Wind Tunnel, full details of which can be found in Johl, Passmore & Render [13]. The operating velocity in the test section was up to 40m/s.…”
Section: Experimental Methodologymentioning
confidence: 99%
“…Testing was performed in the Loughborough University Wind Tunnel, Figure 1, full details of which can be found in [12]. The operating velocity in the test section was 40 m.s -1 .…”
Section: Facilitiesmentioning
confidence: 99%