WIND TUNNEL TEST REPORT CONVENTIONAL MODEL. VOLUME 2. LOW SPEED PRESSURE AND HINGE MOMENTS

Abstract

The report presents the results from wind tunnel tests of a one- eighth scale conventional model of the U. S. Army XV-5A Lift Fan Flight Research Aircraft. Volume II presents hinge moment coefficients and pressure data in plotted and tabular form with pertinent detail explanatory information. Pressure and hinge moment data were not recorded during the second phase of the low speed testing.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1964
Accession Number
AD0653568

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Advanced Electronics
  • Cyber

DTIC Thesaurus Topics

  • Aircrafts
  • Army Aviation
  • Control Surfaces
  • Department Of Defense
  • Flaps (Control Surfaces)
  • Government Procurement
  • Governments
  • Horizontal Stabilizers
  • Landing Gear
  • Model Tests
  • Pressure Transducers
  • Research Aircraft
  • Surfaces
  • Trailing Edges
  • Transducers
  • Wind Tunnel Tests
  • Wing Flaps

Readers

  • Business Analytics
  • Fluid Dynamics.
  • Structural Dynamics.