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Investigation of X24C-2 10-Stage Axial-Flow Compressor (1947)

Buckner, Howard Jr. ; Finger, Harold B. ; Schum, Harold J.

In: CASI

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Publication Date: 2019-08-17

Description: Effect of inlet-air pressure and temperature on the performance of the X24-2 10-Stage Axial-Flow Compressor from the X24C-2 turbojet engine was evaluated. Speeds of 80, 89, and 100 percent of equivalent design speed with inlet-air pressures of 6 and 12 inches of mercury absolute and inlet-air temperaures of approximately 538 degrees, 459 degrees,and 419 degrees R ( 79 degrees, 0 degrees, and minus 40 degrees F). Results were compared with prior investigations.

Keywords: Aircraft Propulsion and Power

Type: NACA-RM-E7H22

Format: application/pdf

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