SUPPLEMENTARY STUDY REPORT ROTOR/WING CONCEPT STUDY

Abstract

The basic data and analyses from the Rotor/Wing wind tunnel tests were reported in HTC-AD 65-15 (AD-473 862L, 863L, 864L). Supplementary analyses of the data with respect to Rotor/Wing rolling and pitching moments in the low- rpm range, Rotor/Wing shaft bending moments in 1-g running-rotor flight, horizontal tail efficiency, and Rotor/Wing blade root bending moments are included in this report.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1966
Accession Number
AD0489862

Entities

People

  • Robert E. Head

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Bending Moments
  • Computer Programs
  • Computers
  • Dynamic Pressure
  • Efficiency
  • Fuselages
  • Helicopters
  • Horizontal Stabilizers
  • Model Tests
  • Propulsion Systems
  • Ship Model Basins
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerodynamics/Aeronautics.
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