James E. Hatch

发表

Effect of Various Blade Modifications on Performance of a 16-Stage High-pressure-ratio Axial-flow Compressor.Angles 3 deg, 1, Effect on Over-all Performance Characteristics of Decreasing Twelfth Through Fifteenth State Stator-blade Angles 3 deg

Arthur A. Medeiros, James E. Hatch, James F. Dugan, 1952 .

Application of radial-equilibrium condition to axial-flow turbomachine design including consideration of change of entropy with radius downstream of blade row

James E. Hatch, Robert J. Jackson, Charles C. Giamati, 1954 .

Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor. III - Effect on Over-All Performance Characteristics on Increasing Stator-Blade Angles in Inlet Stages

Arthur A. Medeiros, James E. Hatch, 1952 .

Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor. II - Effect on Over-All Performance Characteristics of Increasing Twelfth through Fifteenth Stage Stator-Blade Angles 3 deg

Arthur A. Medeiros, James E. Hatch, 1952 .

Performance of a 13-Stage Development Compressor for the J40-WE-24 Engine at Equivalent Speeds from 30 to 112 Percent of Design

James E. Hatch, Harold B. Finger, James G. Lucas, 1953 .

Effect of Various Blade Modifications on Performance of A16-Stage Axial-Flow Compressor. V - Effect on Over-All Performance Characteristics of a 20-Percent Reduction in Solidity of the Fourteenth Through Sixteenth Stage Rotors

Arthur A. Medeiros, James E. Hatch, 1952 .

Performance of J35-A-23 compressor I : over-all performance characteristics at equivalent speeds from 20 to 100 percent of design

Arthur A. Medeiros, James E. Hatch, Donald C Guentert, 1951 .

Use of a Theoretical Flow Model to Correlate Data for Film Cooling or Heating an Adiabatic Wall by Tangential Injection of Gases of Different Fluid Properties

James E. Hatch, S. Stephen Papell, 1959 .