Flow Analysis in Spiked Supersonic Intakes of A/C (I - Inviscid)
The intakes of supersonic aircraft are usually affected by two substantial factors, namely, the “spike” and the “angle of attack”. The aim of the present work is to analyze the flow field structure in the supersonic intakes equipped with spike. The analysis is carried out under the assumption of non...
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| Main Authors: | , |
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| Format: | Conference or Workshop Item |
| Published: |
UPM - Malaysia
2007
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| Subjects: | |
| Online Access: | http://eprints.utp.edu.my/4145/1/FLOW_ANALYSIS_IN_SPIKED_SUPERSONIC_INTAKES_OF_A.pdf http://eprints.utp.edu.my/4145/ |
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