Publication Date:
2019-06-27
Description:
A two-dimensional finite difference numerical technique is presented to determine the temperature distribution in a solid blade of a radial guide vane. A computer program is written in Fortran IV for IBM 370/165 computer. The computer results obtained from these programs have a similar behavior and trend as those obtained by experimental results.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-CR-137633
Format:
application/pdf