Unsteady response of an axial flow compressor to planar temperaturetransients
- 1 January 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (1) , 11-18
- https://doi.org/10.2514/3.45074
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Compressor response to pulsed transientsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Blast from moving gunsJournal of Aircraft, 1977
- Turbomachinery WavesAeronautical Quarterly, 1977
- Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System ModelJournal of Engineering for Power, 1976
- Nonlinear Analysis of Rotating StallJournal of Engineering for Power, 1972
- A unified theory of inlet/engine compatibilityPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972