Publication Date:
2019-08-15
Description:
An investigation was conducted to determine the operational and performance characteristics of the TG-100A gas turbine-propeller engine II. Windmilling characteristics were deterined for a range of altitudes from 5000 to 35,000 feet, true airspeeds from 100 to 273 miles per hour, and propeller blade angles from 4 degrees to 46 degrees.
Keywords:
Aircraft Propulsion and Power
Type:
NACA-RM-E7G25
Format:
application/pdf
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