Publication Date:
2019-08-15
Description:
Wind tunnel investigations were performed to determine the performance properties of an axial-flow gas turbine-propeller engine II. Windmilling characteristics were determined 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-E8F10a
Format:
application/pdf
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