NASA TN D-4421
Louis J. Goldman, Vincent J. Scullin, United States. National Aeronautics and Space Administration, Lewis Research Center
National Aeronautics and Space Administration, 1968 - Turbomachines
13 pages matching blade design in this book
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ALPHUO angle from separation array for storing BETAN blade design blade spacing calculated CALL ROOT circular arc point computer program dimensionless equation FKMAX flow direction flow separation flow turning FOFX FUNCTION GAMM1 GSTAR inlet and outlet inlet flow angle inlet transition arc INPUT IPRINT JDEX KDEX kmax KNDEX KOUNT lower transition arc LSTR GT Mach line maximum weight flow MAXN MAXO method of characteristics MSSTAR number of points outlet flow angle outlet transition arc output parameters PHIKP1 printed radius separation criterion specific-heat ratio SSMLOW SSMUP starting and flow storage for values storing X*-coordinate straight-line portion subroutine ROOT supersonic blade sections supersonic starting surface Mach number TANBO temporary storage transition arc points unrotated upper transition arc upper-curve upper-surface Prandtl-Meyer angle variable index velocity ratio VLOW vortex flow wall segments XDOWN(L XINTL XSOUT XUPN(l Y*-coordinate YACRS2(M YACRSKL YLOWO(LSTR