Investigation of a Highly Loaded Two-Stage Fan-Drive Turbine. Volume III. Phase II, Part 2. Experimental Baseline Airfoil Evaluation.

Abstract

The design of the cascade hardware and baseline airfoils was previously reported. The test results of baseline airfoil performance in the annular cascade and the status of the other tasks are presented in this report.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1969
Accession Number
AD0506871

Entities

People

  • Donald E. Dahlberg
  • Henry Welna
  • William H. Heiser

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Boundary Layer Control
  • Flow
  • Flow Visualization
  • Gas Flow
  • Governments
  • Guide Vanes
  • Inlet Guide Vanes
  • Layers
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Measurement
  • Static Pressure
  • Test And Evaluation
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Software Engineering