Difficulty: Easy
Correct Answer: Incorrect
Explanation:
Introduction / Context:
Compressors are categorized by the direction of primary flow relative to the machine axis. Correct classification matters for predicting performance maps, surge behavior, and stage loading limits.
Given Data / Assumptions:
Concept / Approach:
A centrifugal compressor accepts flow near the center and imparts tangential velocity, flinging the fluid radially outward; static pressure then increases in a diffuser. An axial-flow compressor compresses the fluid while it moves axially through alternating rows of rotating and stationary blades. The flow directions and stage architectures are fundamentally different.
Step-by-Step Solution:
Verification / Alternative check:
Standard turbomachinery texts depict velocity triangles: centrifugal has a large radial component at impeller exit, while axial maintains nearly axial absolute velocity through stages.
Why Other Options Are Wrong:
Conditional “correct” options attempt to blur definitions; even with vaneless diffusers or multishaft layouts, the primary flow direction in centrifugal stages remains radial, not axial.
Common Pitfalls:
Confusing “mixed-flow” compressors with pure axial or pure centrifugal designs.
Final Answer:
Incorrect
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