Investigation of the vortical flow around a reverse delta wing
A six component force balance was used to obtain the CL for a reverse delta wing and a delta wing for comparison purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta...
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| தலைமை எழà¯à®¤à¯à®¤à®¾à®³à®°à¯à®•ளà¯: | , , , |
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| வடிவமà¯: | Conference or Workshop Item |
| மொழி: | English |
| வெளியீடபà¯à®ªà®Ÿà¯à®Ÿà®¤à¯: |
2011
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| பகà¯à®¤à®¿à®•ளà¯: | |
| நிகழà¯à®¨à®¿à®²à¯ˆ அணà¯à®•லà¯: | http://irep.iium.edu.my/2364/ http://irep.iium.edu.my/2364/ http://irep.iium.edu.my/2364/1/paper_4.pdf |
| கà¯à®±à®¿à®¯à¯€à®Ÿà¯à®•ளà¯: |
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| தொகà¯à®ªà¯à®ªà¯: | A six component force balance was used to obtain the
CL for a reverse delta wing and a delta wing for comparison
purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta wing. |
|---|