Noise Survey Under Static Conditions of a Turbine-driven Full-scale Modified Supersonic Propeller with an Advance Ratio of 3.2
1958-01-01
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Englisch
Noise survey of 10-foot four-blade turbine-driven propeller under static conditions
Engineering Index Backfile | 1955
|Effect of advance ratio on flight performance of modified supersonic propeller
Engineering Index Backfile | 1958
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