Analytical Investigation of Supersonic Turbomachinery Blading, Volume 1National Aeronautics and Space Administration, 1968 - Turbomachines |
Common terms and phrases
ALFUNC ALPHLO ALPHUP ALPLOW array for storing BETAN BETAT blade design calculated CALL ROOT circular arc COMMON/FACTOR/PERM coordinates dimensionless equation flow separation flow turning FOFRS FOFX FORMAT FUNC FUNCTION GAMM1 GAMP1 GSTAR inlet and outlet inlet transition arc INPUT IPRINT EQ JDEX+1 KDEX Kmax KOUNT lower transition arc lower-curve lower-surface LSTR GT Mach line Mach number maximum weight flow MAXN MAXO MSSTAR number of points outlet transition arc output parameters Prandtl-Meyer angle RECONV RETURN END IBFTC RLOW rotated separation criterion specific-heat ratio SSMLOW SSMUP subroutine ROOT supersonic starting surface Mach number TANBO temporary storage transition arc points unrotated upper transition arc upper-curve variable index velocity ratio VIMAX VLOW vortex vortex flow VOUT WRITE XDOWN XDOWN(L XINTL XLOW XLOWN XLOWO XSOUT XUPN Y*-coordinate YACRS1 YLOW YLOWN YLOWO YUP JDEX YUPN YUPO