Theuniformairflowapproachingtheairfoilisgeneratedbyano

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: expansion fan doing the turning, relative to the nozzle centerline. e. Determine the Mach number and temperature of the flow after this initial turn. 3. A flat plate airfoil is placed in a supersonic wind tunnel at an angle of attack of 18 degrees. The uniform air flow approaching the airfoil is generated by a nozzle with an exit to throat area ration of 5.3 exhausting air from a chamber where the tempera...
View Full Document

Ask a homework question - tutors are online