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Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber with Development of an Optimized Design

Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber with Development of an Optimized Design

by NationalAeronauticsandSpaceAdministr (Creator), Mary F . Wadel (Author)

$48.10

Quantity

10 in stock

More Information

Format: Paperback
 Pages: 82
 Publisher: BiblioScholar
Published: 12 Mar 2013
ISBN 10: 1288910762
ISBN 13: 9781288910762