1137602

SAE ARP996A

COOLING DATA FOR TURBINE ENGINES IN HELICOPTERS

standard by SAE International , 01/31/2020

View all product details

Most Recent

Track It

Language:
    • Available Formats
    • Options
    • Availability
    • Priced From ( in USD )
    • Printed Edition
    • Ships in 1-2 business days
    • $129.00
    • Add to Cart
    • Printed Edition + PDF
    • Immediate download
    • $168.00
    • Add to Cart

Customers Who Bought This Also Bought

 

About This Item

 

Full Description

Efficient design of a turbine engine installation requires data on the ways the engine rejects heat, the temperature limits of various parts of the engine, and the changes in heat rejection from service, as well as a method of using these data. A uniform, practical method of data presentation and use is needed. Cooling margins developed by these methods would be subject to full scale testing for verification. A tested method of data presentation and use is described herein.
 

Product Details

Published:
01/31/2020
File Size:
1 file , 5.3 MB
Note:
This product is unavailable in Ukraine, Russia, Belarus