Experimental Study of Slot Injection into a Supersonic Stream

• 1 May 1973
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
• Vol. 11  (5) , 585-586
• https://doi.org/10.2514/3.50497

Abstract

Keywords

• SKIN FRICTION
• DATA ACQUISITION
• PRESSURE GRADIENTS
• SUPERSONIC SPEED
• TURBULENT BOUNDARY LAYER