Search U.S. government technical reports digitized or harvested by TRAIL.

Keyword Search

Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade

NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results

A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed

Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading

A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05

Published Year

• 1950-1959 (5)

Subject

• Cascades (Fluid dynamics) (5) *
• Axial flow compressors--Blades (3)
• Compressors--Blades (2)
• Compressors--Performance (2)
• Aerodynamic load (1)
• Aerofoils (1)
• Air ducts (1)
• Air flow (1)
• Charts, diagrams, etc (1)
• Gas-turbines--Blades (1)
• Reynolds number (1)
• Turbomachines--Blades (1)

Author

• Emery, James C. (2)
• Erwin, John R. (2)
• Ashby, George C. (1)
• Connors, James F. (1)
• Felix, A. Richard. (1)
• Godwin, William R. (1)
• Meyer, Rudolph C. (1)
• Savage, Melvyn. (1)
• Schulze, Wallace M. (1)
• Westphal, Willard R. (1)

• About TRAIL
• FAQ
• Join TRAIL
• Contact Us

Search developed and maintained by the University of Washington Libraries
Copyright 2010