Wind Tunnel Test Data Report of a Powered 1/5 Scale ARL/Bell V/STOL Aircraft Model. Phase II,

Abstract

Tests of a 1/5 scale powered V/STOL aircraft model were conducted in the Langley 7 x 10 wind tunnel. Vehicle aerodynamics and stability and control characteristics were investigated. The test results are presented without analysis.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1969
Accession Number
ADA012094

Entities

People

  • A. T. Hesby
  • C. Henderson
  • P. E. Ryan
  • R. M. Breidenstein

Organizations

  • Bell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamics
  • Aircraft Models
  • Aircrafts
  • Models
  • Short Takeoff Aircraft
  • Vehicles
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering