Accession Number:

ADA067703

Title:

Design of Shock-Free Transonic Flow in Turbomachinery.

Personal Author(s):

Corporate Author:

NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF

Report Date:

1978-11-01

Abstract:

A new design method for transonic flow in turbomachinery is described. The idea is based on the authors previous experience with hodograph methods but carried out in physical space. If combined with a flow analysis code the new method can be used as a designanalysis tool. Results illustrating this procedure are given for two dimensional flow through cascades and past airfoils. Existing configurations can be made shock-free by computational modifications which are limited to that portion of the design shape which is wetted by supersonic flow. Author

Descriptive Note:

Technical rept. 20 Jun-15 Aug 78,

Pages:

0041

Descriptors:

Identifiers:

Subject Categories:

Communities Of Interest:

Modernization Areas:

File Size:

12.79MB

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