Publication Date:
2011-08-16
Description:
Direct skin friction measurements obtained on the wall of a Mach 19.8 nozzle are presented. These measurements of skin friction and values deduced from the profile data are compared with predictions from a finite difference theory and also with several 'flat-plate' prediction methods for skin friction.
Keywords:
AERODYNAMICS
Type:
AIAA Journal; 10; Sept
Format:
text