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L. R. Woodworth

The Significance of Major Cycle Variables on Turbojet Engine Performance at Mach 3.0

1955
Approximate methods for determining the performance of gas turbine engines at off-design conditions.

1954
Performance analysis methods for the twin-spool, high-pressure ratio, turbojet engine.

1952
The generalized approach to the selection of propulsion systems for aircraft.

1951
Gas Turbine Cycle Analysis by Means of Entropy Changes and Polytropic Component Efficiencies

1949