STUDY OF TURBINE AND TURBOPUMP DESIGN PARAMETERS. VOLUME 1. A STUDY OF HIGH PRESSURE RATIO RE-ENTRY TURBINES Open PDF Document Details Document Type Technical Report Publication Date Jan 30, 1960 Accession Number AD0232635 Entities People Hans D. Linhardt Tags Communities of Interest Air Platforms DTIC Thesaurus Topics Accuracy Altitude Chambers Boundaries Boundary Layer Calibration Coefficients Computational Fluid Dynamics Flow High Altitude High Pressure Instrumentation Lepidoptera Mach Number Measurement Pressure Measurement Static Pressure Three Dimensional