Work

Engine investigation of an air-cooled turbine rotor blade incorporating impingement-cooled leading edge, chordwise passages, and a slotted trailing edge

Year: 1972

Type: article

Source: NASA Technical Reports Server (NASA)

Authors: R. P. Dengler, F. C. Yeh, J. W. Gauntner, G. E. Fallon

Institution: Glenn Research Center

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

SDG: Affordable and clean energy

Open Access status: closed

OpenAlex ID: W748623323

FWCI: 7.5

Cites: 3

Cited by: 5

Related to: 10