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- Matching Characteristics of J35-A-23 Compressor and Two-stage Turbine
- Sea-level static equilibrium performance of actual two-spool turbojet engine and comparison with hypothetical engine
- Two-Spool Matching Procedures and Equilibrium Characteristics of a Two-Spool Turbojet Engine
- Effect of Design Compressor Pressure Ratio on Performance of Hypothetical Two-Spool Nuclear-Powered Turbojet Engines
- Component Operating Trends During Acceleration and Deceleration of Two Hypothetical Two-Spool Turbojet Engines
- Performance and Component Frontal Areas of a Hypothetical Two-Spool Turbojet Engine for Three Modes of Operation
- Comparison of Performance and Component Frontal Areas of Hypothetical Two-Spool and One-Spool Turbojet Engines
- Investigation of Rotating-Stall Limits in a Supersonic Turbofan Engine
- Effect of Design Variables on Performance of Mach 4.0 Hydrogen Expansion Engines
- Effect of Design Variables on Performance of Mach 4.0 Hydrogen Expansion Engines