Dynamic investigation of turbine-propeller engine under altitude conditions

Krebs, Richard R., Himmel, Seymore C., Blivas, Darnold., Shames, Harold.
naca-rm-e50j24
1950


An altitude-wind-tunnel investigation of the dynamics of a turbine-propeller engine employing the frequency-response technique was conducted over a range of pressure altitudes from 10,000 to 30,000 feet.

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