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Summary of Investigations of Mark 25 Aerial-Torpedo Turbine (1950)

Schum, Harold J. ; Whitney, Warren J. ; Buckner, Howard A., Jr.

In: CASI

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Publication Date: 2019-07-11

Description: The power plant from a Mark 25 aerial torpedo was investigated both as a two-stage turbine and as a single-stage modified turbine to determine the effect on overall performance of nozzle size and shape, first-stage rotor-blade configuration, and axial nozzle-rotor running clearance. Performance was evaluated in terms of brake, rotor, and blade efficiencies. All the performance data were obtained for inlet total to outlet static pressure ratios of 8, 15 (design), and 20 with inlet conditions maintained constant at 95 pounds per square inch gage and 1000 F for rotor speeds from approximately 6000 to 18,000 rpm.

Keywords: Aircraft Propulsion and Power

Type: NACA-RM-SE50D12

Format: application/pdf

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