28.02.2013 Views

Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

<strong>of</strong> the component designers must be accounted for. Once the s<strong>of</strong>tware is in<br />

production as a design tool, the ongoing costs and manpower resources<br />

necessary to maintain and upgrade an in-house program throughout its life<br />

cycle must also be addressed. In contrast, when commercial s<strong>of</strong>tware is<br />

leased or purchased, program upgrades and maintenance services from the<br />

vendor are <strong>of</strong>ten included.<br />

Therefore, except in those circumstances when no commercial<br />

s<strong>of</strong>tware packages meet the specifications for the CFD analysis tool, or<br />

when it is recognized that other special requirements would dictate in-house<br />

development, it would <strong>of</strong>ten be more cost-effective to acquire a commercial<br />

s<strong>of</strong>tware product.<br />

FUTURE EXPECTATIONS<br />

The preceding sections <strong>of</strong> this chapter have presented a view <strong>of</strong> the<br />

characteristics <strong>of</strong> turbomachinery flow fields and the current status <strong>of</strong><br />

analysis techniques used to model these flows. In the following paragraphs,<br />

an attempt will be made to focus on the trends that appear to be developing,<br />

as a result <strong>of</strong> the increasingly strong interrelationship between the<br />

aerodynamic design <strong>of</strong> turbomachinery components and the ability to<br />

realistically model and analyze the flow fields associated with those<br />

components.<br />

Trends in Component Design<br />

A primary driver determining the trends in turbomachinery component<br />

design in the near future will be the IHPTET program. With its goal <strong>of</strong><br />

doubling propulsion engine performance capability by the year 2003,<br />

relative to 1980s base technology levels, revolutionary advances will be<br />

achieved in terms <strong>of</strong> reductions in specific fuel consumption (SFC) and<br />

increases in power-to-weight or thrust-to-weight ratios. As an example [79],<br />

for turbine engines in the small/medium size class, the IHPTET goals are to<br />

reduce SFC by 30% and increase power-to-weight ratio by 100%. In<br />

addition to these performance improvements, the engines are expected to be<br />

approximately 70% smaller in diameter and weight than 1980s technology<br />

engines.<br />

While IHPTET represents revolutionary technology, the advances<br />

achieved along the way to the final goals will be progressively implemented<br />

in existing or new engine applications to improve performance. Thus, the<br />

benefits <strong>of</strong> this advanced technology program will be appearing in the design<br />

<strong>of</strong> commercial and military engines long before the program’s conclusion in<br />

Copyright © 2003 Marcel Dekker, Inc.

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!