Increasing the Range of Axial-Flow Compressors by Use of Adjustable Stator Blades
- 1 May 1947
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 14 (5) , 269-282
- https://doi.org/10.2514/8.1347
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Characteristics of Airfoils in a Cylindric Axial-Flow GridJournal of the Aeronautical Sciences, 1943