WIND TUNNEL TEST REPORT CONVENTIONAL MODEL. VOLUME 1. LOW SPEED FORCE AND MOMENT DATA

Abstract

The report presents the results from the wind tunnel tests of a 1/8- scale conventional model of the U. S. Army XV-5A Lift Fan Flight Research Aircraft. The tests were performed to determine the subsonic aerodynamic characteristics of the XV-5A in its conventional flight configuration. Volume I contains the tabulated force and moment data from the low speed (M = 0.285) tests.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1964
Accession Number
AD0653566

Entities

Organizations

  • General Electric

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Army Aviation
  • Aspect Ratio
  • Control Surfaces
  • Dynamic Pressure
  • Government Procurement
  • Governments
  • Horizontal Stabilizers
  • Landing Gear
  • Measurement
  • Model Tests
  • Research Aircraft
  • Ship Model Basins
  • Test Facilities
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Dynamics.