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- Tests of two models representing intermediate inboard and outboard wing sections of the XB-36 airplane
- Wind-Tunnel Investigation of a Low-Drag Airfoil Section with a Double Slotted Flap
- Blade Design Data for Axial-Flow Fans and Compressors
- Performance of compressor blade cascades at high Mach numbers
- Axial-flow fan and compressor blade design data on 52.5 degrees stagger and further verification of cascade data by rotor tests
- Performance of axial-flow fan and compressor blades designed for high loadings