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Flugtriebwerk
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Altitude Performance of J35-A-17 Turbojet Engine in an Altitude Chamber
Altitude Performance and Operational Characteristics of YJ71-A-7 Turbojet Engine
Aspects of Internal-Flow-System Design for Helicopter Propulsive Units
Over-All Performance of J65-B3 Turbojet Engine for Reynolds Number Indices from 0.8 to 0.2
Progress Report for the Month of September 1957
Suggested Preliminary Design Program for Pwar-11
System 125A: Preliminary Radiation Effects Analysis, (Tarpon) Experimental Airplane