ON THE VISCOUS VERSUS NON-VISCOUS FLOW ANALYSIS IN SUPERSONIC SPIKED INTAKES

• Main Authors: Al-Kayiem, Hussain H., Salih, T. W., Al-Ambari, A. S. S.
• Format: Conference or Workshop Item
• Published: 2010
• Subjects: TJ Mechanical engineering and machinery; U Military Science (General); TL Motor vehicles. Aeronautics. Astronautics
• Online Access: http://eprints.utp.edu.my/4242/1/WEC_2010_CAME_7_viscous_versus_non_1_page_.pdf; http://eprints.utp.edu.my/4242/

The supersonic flow approaching the intake of a supersonic aero engine must be brought to subsonic state before reaching the compressor face stage. The velocity reduction is combined with reduction in the total pressure of the flow, which is not preferable by the designer of the supersonic gas turbi...