A method for calculating inlet distortion effects on stability of split-flow fans.
- Published in:
- Aeronautical Journal, 2009, v. 113, n. 1147, p. 591, doi. 10.1017/S0001924000003250
- By:
- Publication type:
- Article
Works matching DE "TURBOJET plane engine compressors"
Results: 2
1
2
Numerical Parametric Study of Inlet Distortion Propagation in Compressor Using Integral Approach with Taguchi Method.
- Published in:
- International Journal for Computational Methods in Engineering Science & Mechanics, 2005, v. 6, n. 3, p. 169, doi. 10.1080/15502280590923676
- By:
- Publication type:
- Article