Wind Tunnel Test of the Aerodynamics and Dynamics of Rotor Spinup, Stopping and Folding on a Semispan Folding Tilt-Rotor Model. Volume VII

Abstract

Wind tunnel test data obtained with a 1/9-scale semispan, unpowered, dynamically-scaled Model 213 stowed/tilt rotor are reported. The objectives of the tests were to obtain aerodynamic, structural, and dynamics data during the spinup, feather and blade fold cycles of this vehicle.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1971
Accession Number
AD0736825

Entities

People

  • Dirk Van Wagensveld
  • Frank J. Mchugh
  • John P. Magee
  • Leon N. Delarm
  • Walter L. Lapinski

Organizations

  • Boeing Rotorcraft Systems

Tags

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Air Force
  • Aircraft Equipment
  • Aircrafts
  • Airfoils
  • Airframes
  • Autorotation
  • Contracts
  • Data Analysis
  • Design Criteria
  • Frequency
  • Horizontal Stabilizers
  • Spars
  • Tilt Rotor Aircraft
  • Wind Tunnel Tests
  • Wind Tunnels
  • Wing Flaps

Fields of Study

  • Physics

Readers

  • Aerospace Engineering