
Accession Number : AD0656428
Title : A METHOD OF CALCULATING QUASI TWODIMENSIONAL FLOWS THROUGH CASCADES,
Corporate Author : CALIFORNIA INST OF TECH PASADENA HYDRODYNAMICS LAB
Personal Author(s) : Mani,Ramani
Report Date : JUL 1967
Pagination or Media Count : 48
Abstract : Details are given of a procedure to compute the effect of varying axial velocity on the cascade performance of an axial flow compressor blade row. The relevant equations and the procedure of solution are given. Details are given of a computing program to carry out the calculations. The program is written in Fortran IV and is in three parts. Data cards giving details of the flow geometry have to be punched for the first part only. (Author)
Descriptors : (*AXIAL FLOW COMPRESSORS, TWO DIMENSIONAL FLOW), CASCADE STRUCTURES, GAS FLOW, AIRFOILS, MATHEMATICAL ANALYSIS, COMPUTER PROGRAMS
Subject Categories : Aerodynamics
Fluid Mechanics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE