Flow Analysis in Spiked Supersonic Intakes of A/C (I - Inviscid)

• Main Authors: Al-Kayiem, Hussain H., Al-Ambari, A.S.S
• Format: Conference or Workshop Item
• Published: UPM - Malaysia 2007
• Subjects: TJ Mechanical engineering and machinery; U Military Science (General); TL Motor vehicles. Aeronautics. Astronautics
• Online Access: http://eprints.utp.edu.my/4145/1/FLOW_ANALYSIS_IN_SPIKED_SUPERSONIC_INTAKES_OF_A.pdf; http://eprints.utp.edu.my/4145/
• Institution: Universiti Teknologi Petronas

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...