TABULATED SIKORSKY CH-34 BLADE SURFACE PRESSURES MEASURED AT THE NASA/ AMES FULL SCALE WIND TUNNEL

Abstract

Tests were conducted on a full scale Sikorsky CH-34 rotor blade system, instrumented to measure chordwise pressure distributions. The basic pressure measurements are presented in tabular form to make the detailed data available for possible analysis.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 15, 1966
Accession Number
AD0634952

Entities

People

  • A. A. Lizak
  • J. P. Rabbott Jr.
  • V. M. Paglino

Organizations

  • United Technologies Corporation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acquisition
  • Aircrafts
  • Army Aviation
  • Control Systems
  • Data Acquisition
  • Data Processing
  • Digital Information
  • Government Procurement
  • Governments
  • Instrumentation
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Recording Systems
  • Stations
  • Two Dimensional
  • Wind Tunnels

Readers

  • Aerodynamics.
  • Aerospace Engineering
  • Fluid Dynamics.