Radial Turbine Preliminary Aerodynamic Design Optimization for Expander Cycle Liquid Rocket Engine

doi 10.2514/6.2006-5046
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy