Browse TRAIL Inventories

Turning-Angle Design Rules for Constant-Thickness Circular-Arc Inlet Guide Vanes in Axial Annular Flow

Compressibility Correction for Turning Angles of Axial-Flow Inlet Guide Vanes

Secondary Flows in Annular Cascades and Effects on Flow in Inlet Guide Vanes

Experimental investigation of an axial flow compressor inlet stage operating at transonic relative inlet Mach numbers I : over-all performance of stage with transonic rotor and subsonic stators up to rotor relative inlet Mach number of 1.1

Theoretical and Experimental Analysis of One-Dimensional Compressible Flow in a Rotating Radial-Inlet Impeller Channel

Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers III : blade-row performance of stage with transonic rotor and subsonic stator at corrected tip speeds of 800 and 1000 feet per secon

Diffusion factor for estimating losses and limiting blade loadings in axial-flow-compressor blade elements

Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers IV : stage and blade-row performance of stage with axial-discharge stators

Review of High-Performance Axial-Flow-Compressor Blade-Element Theory

Aerodynamic Design of Axial-flow Compressors 6 - Experimental Flow in Two-Dimensional Cascades

Theoretical Loss Relations for Low-Speed Two-Dimensional-Cascade Flow

Low-Speed Wake Characteristics of Two-Dimensional Cascade and Isolated Airfoil Sections

Analysis of experimental low-speed loss and stall characteristics of two-dimensional compressor blade cascades

Analytical relation for wake momentum thickness and diffusion ratio for low-speed compressor


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