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Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas

Title:Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas
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Note:National Advisory Committee for Aeronautics, 1957
  
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Subject:Air flow
Subject:Airplanes -- Turbojet engines
Subject:Charts, diagrams, etc.
Subject:Combustion chambers
Subject:Mathematics
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