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Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800 degrees R

Title:Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800 degrees R
Alternate title:Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800° R
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Note:National Advisory Committee for Aeronautics, 1948
  
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Subject:Aeronautics -- Research
Subject:Aircraft gas-turbines
Subject:Gas turbines
Subject:Gas-turbines
Subject:Gas-turbines -- Aerodynamics
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