Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
14 results returnedSearch results
- 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