STUDY OF TURBINE AND TURBOPUMP DESIGN PARAMETERS. VOLUME 1. A STUDY OF HIGH PRESSURE RATIO RE-ENTRY TURBINES

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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