Calculation of the Aerodynamic Loading on the Blade of a Main Rotor in the General Case of Helicopter Flight,

Abstract

Expressions for calculating the aerodynamic loading on a helicopter rotor blade are derived for the general case of helicopter flight along some curvilinear trajectory. A one-rotor helicopter scheme is examined. Rotor blade-fuselage interaction is not considered.

Document Details

Document Type
Technical Report
Publication Date
Apr 30, 1975
Accession Number
ADA014047

Entities

People

  • A. K. Yanko
  • A. N. Bazilevskii
  • I. G. Pavlov

Organizations

  • United States Army Foreign Science and Technology Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Loading
  • Aircrafts
  • Airframes
  • Fuselages
  • Helicopter Rotors
  • Helicopters
  • Mechanical Structure
  • Rotary Wing Aircraft
  • Trajectories
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Dynamics.