Correlation of Data Related to Shock-induced Trailing-edge Separation and Extrapolation to Flight Reynolds Number |
From inside the book
72 pages matching flight Reynolds number in this book
Where's the rest of this book?
Results 1-3 of 72
Common terms and phrases
AEDC 16T angle of attack B1/2 FIGURE base boundary layer characteristics chord collapse comparison complete COMPOSITE CORRELATION concept CONFIGURATION consideration correlation curves correlation parameter CPSH CPTE CPTE CPTEO CRITERIA defined differences discussed extrapolation fact factor Figure 46 FINAL CORRELATION flight data flight Reynolds number Flow forward full scale high Reynolds number higher illustrated increased indicated influence INITIAL CORRELATION leading low Reynolds number Mach number measured obtained occurs parameter B1/2 plotted points possibility predicted present pressure coefficient pressure distribution previously procedure RAE MODEL 864 range Reference Report scale effect scatter separation development shape shock location shock pressure rise shown in Figure significant similar slope SOURCE RN-106 SYM spacing spanwise station speed supercritical tests tion trailing edge trailing-edge pressure recovery trailing-edge separation transition transonic TYPICAL values variation vortex wind tunnel data wing XCSH Ср