High Reynolds Number Tests of a C-141A Aircraft Semispan Model to Investigate Shock-induced Separation |
Common terms and phrases
16T TRANSITION FIXED 20 REYNOLDS NUMBER 75 RNCE AEDC 16T TRANSITION airfoil ALPHA D+XO angle of attack boundary layer C-141 SEMI-SPAN MODEL CFF SMOOTH AEDC CFF TRANSITION FIXED CH141 SEMI-SPAN Compressible Flow Facility configuration correlation CPTE D+ XO D+XO A ALPHA degree angle element line figures 12 FIXED CFF SMOOTH FLIGHT REFERENCE flight test FLOOR SEALED FREE PAGE FIGURE high Reynolds number highest Reynolds number Lockheed-Georgia Company low Reynolds numbers LSHT 10 DATE LSHT DATE Mach number MODEL 80 RNCE MODEL ME 825 outboard stations OX+A panel model porosity pressure coefficient pressure distribution pylons and nacelles scale effects SEMI-SPAN MODEL 80 semispan test shock location shock-induced separation SMOOTH AEDC 16T SPAN MODEL span wise contamination spanwise station STA 389 FREE stagnation pressure station 389 station 637 trailing-edge pressure recovery trailing-edge separation TRANSITION FIXED CFF TRANSITION FIXED REFERENCE transonic wind tunnel wing X/CSH XO ALPHA