Work

Starting Characteristics of a Convergent-divergent Diffuser Blade Passage of a Supersonic Compressor in Mach Three Flow,

Year: 1960

Type: article

Source: Defense Technical Information Center (DTIC)

Authors: Agosta,Vito D., DeCarlo,Joseph P.

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W218535385

FWCI:

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Related to: 10