|
|
SiteMap
|
You are here: home->amp->B02->B.8.1.9.4.A.1
8194
(1) In a turbine engine axial flow compressor, each consecutive pair of rotor and stator blades constitutes a pressure stage.
(2) In a turbine engine axial flow compressor, the number of rows of stages is determined by the amount of air and total pressure rise required.
Regarding the above statements,
| | A) only No. 1 is true. |
| | B) only No. 2 is true. |
| | C) both No. 1 and No. 2 are true. |
|
|
|
|
