The Two Dimensional Inflow Conditions for a Supersonic Compressor With Curved Blades

doi 10.21236/ad0101949
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Defense Technical Information Center

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy